Digitale Landesbibliothek Berlin Logo

Investigation of atomization characteristics of a dual-swirl centrifugal nozzle in a combustor environment / Liu, Kai (Rights reserved)

Access restriction

Eingeschränkter Zugang mit Nutzungsbeschränkungen: Das Dokument ist in den Räumen der Zentral- und Landesbibliothek mit dem "Virtuellen Lesesaal der Landesbibliothek" auf allen Internet-Arbeitsplätzen zugreifbar, darf jedoch nicht kopiert, versendet oder in einem Umfang von mehr als 10% ausgedruckt werden. Weitere Informationen.

Copyright

No licence for use has been granted - all rights reserved.

Bibliographic data

fullscreen : Investigation of atomization characteristics of a dual-swirl centrifugal nozzle in a combustor environment / Liu, Kai (Rights reserved)

Access restriction

Eingeschränkter Zugang mit Nutzungsbeschränkungen: Das Dokument ist in den Räumen der Zentral- und Landesbibliothek mit dem "Virtuellen Lesesaal der Landesbibliothek" auf allen Internet-Arbeitsplätzen zugreifbar, darf jedoch nicht kopiert, versendet oder in einem Umfang von mehr als 10% ausgedruckt werden. Weitere Informationen.

Copyright

No licence for use has been granted - all rights reserved.

Files

Restricted access: The document can be accessed only at the computer workstations of the Zentral- and Landesbibliothek Berlin. Here you can find our current opening hours.

Unlock

Investigation of atomization characteristics of a dual-swirl centrifugal nozzle in a combustor environment / Liu, Kai (Rights reserved)

You can request access to this file here. You will receive an e-mail confirming that we have successfully received your request.

Investigation of atomization characteristics of a dual-swirl centrifugal nozzle in a combustor environment / Liu, Kai (Rights reserved)

The access to this file is restricted.

What is the first letter of the word "tree"?:

I hereby confirm the use of my personal data within the context of the enquiry made.

Monograph

Title:
Verzeichnis der Büchersammlung der Kaiser Wilhelms-Akademie für das militärärztliche Bildungswesen
Edition:
Dritte Ausgabe
Publication:
Berlin: Verlag von August Hirschwald, 1906
Language:
German
Digitization:
Berlin: Zentral- und Landesbibliothek Berlin, 2023
Scope:
XI, 1055 Seiten
Note:
Die Provenienzmerkmale, die in einzelnen Objekten vorhanden sind, werden derzeit vom Referat Provenienzforschung der ZLB geprüft.
Berlin:
B 540 Wissenschaft. Forschung: Universitäten, Hochschulen, Fachhochschulen
DDC Group:
000 Allgemeines, Wissenschaft
URN:
urn:nbn:de:kobv:109-1-15480004
Collection:
Education,School,Science,Research
Location:
Zentral- und Landesbibliothek Berlin
Shelfmark:
B 540 Kais 5
Copyright:
Public Domain
Accessibility:
Free Access
Title:
Verzeichnis der Büchersammlung der Kaiser Wilhelms-Akademie für das militärärztliche Bildungswesen
Edition:
Dritte Ausgabe
Publication:
Berlin: Verlag von August Hirschwald, 1906
Language:
German
Digitization:
Berlin: Zentral- und Landesbibliothek Berlin, 2023
Scope:
XI, 1055 Seiten
Note:
Die Provenienzmerkmale, die in einzelnen Objekten vorhanden sind, werden derzeit vom Referat Provenienzforschung der ZLB geprüft.
Berlin:
B 540 Wissenschaft. Forschung: Universitäten, Hochschulen, Fachhochschulen
DDC Group:
000 Allgemeines, Wissenschaft
URN:
urn:nbn:de:kobv:109-1-15480004
Collection:
Education,School,Science,Research
Location:
Zentral- und Landesbibliothek Berlin
Shelfmark:
B 540 Kais 5
Copyright:
Public Domain
Accessibility:
Free Access

Chapter

Title:
Medizin. Allgemeine und zusammenfassende Werke
Title:
Medizin. Allgemeine und zusammenfassende Werke

Contents

Table of contents

  • International journal of turbo and jet engines (Rights reserved)
  • Corrigendum to: Aerodynamic performance enhancement of drooped wedge configurations in transonic flow through design optimization / Rinchu, P. (Rights reserved)
  • Effect of micro vortex generator with curved walls on shock boundary layer interaction / Chopde, Rahul S. (Rights reserved)
  • Experimental study on flow field measurements inside the tip clearance of an axial compressor using PIV / Xue, Zhiliang (Rights reserved)
  • Investigation of fluid-induced vibration caused by low engine order total pressure distortions / Chen, Huayin (CC BY)
  • Overall performance analysis of pulse detonation turbofan engine / Zhang, Jiabo (Rights reserved)
  • Multi-modal shroud damping vibration reduction design based on the improved whale optimization algorithm and the energy method / Yuanyuan, Jiang (Rights reserved)
  • Research on a coupling characteristic analysis method for aero-engine considering the influence of S-shaped intake ports / Li, Zeyu (Rights reserved)
  • Experimental and numerical investigation on flow and heat transfer characteristics of swirl cooling with ribs / Xiao, Kun (Rights reserved)
  • Investigation of atomization characteristics of a dual-swirl centrifugal nozzle in a combustor environment / Liu, Kai (Rights reserved)
  • Research on fuel injection strategies on mode transition characteristics for scramjet engine / Zhang, Jian (Rights reserved)
  • Influence of contact stresses in impellers joints on the marine gas turbine rotor stress-strain state / Smetankina, Natalia (Rights reserved)
  • Wall ramp-induced flow modulation in a two-strut hydrogen-fueled scramjet: a numerical study / Dutta, Nilanjana (Rights reserved)
  • Influence of rib parameters on top and sidewalls on particulate deposition and heat transfer in turbine blade cooling passages / He, Hongbin (Rights reserved)
  • Research on multi-parameter optimization methods of the performance for a micro pneumatic turbine / Jin, Jie (Rights reserved)
  • Uncertainty propagation for transient heat transfer in a hollow cylinder / Gorla, Rama Subba Reddy (Rights reserved)
  • Conceptual cooling of superconducting motors in futuristic cryo-electric aviation using gaseous hydrogen / Dhandapani, Anusri (Rights reserved)
  • Computational study of aerodynamic effects in multi-propeller distributed propulsion aircraft / Mistry, Anjali (Rights reserved)
  • Simulation study on the dynamic characteristics and performance laws of a ramjet engine variable-structure-geometry nozzle / Zhao, Hao-Yang (Rights reserved)
  • Effects of trigonometric ripples on flow separation control in rectangular S-ducts / Wang, Yuqi (Rights reserved)
  • Frontmatter (Rights reserved)
  • Aerodynamic performance enhancement of drooped wedge configurations in transonic flow through design optimization / Rinchu, P. (Rights reserved)
  • Hybrid thermodynamic and CFD modeling of a UAV-class micro gas turbine engine: performance validation and optimization / Chauhan, Swati (Rights reserved)
  • Design of accurate integrated torque metering system for determining the fan efficiency of a turbofan engine / Yepifanov, Sergiy (Rights reserved)
  • Research on the control method of turbine outlet temperature limitation protection based on nonlinear state estimation / Liu, Yuan (Rights reserved)
  • Analysis and optimization study on mode transition performance of Ma0-4 parallel TBCC combined engine / Luo, Yi (Rights reserved)
  • Experimental design of counter-flow vortex tubes with varying diameters for multi-nozzle at high-pressure applications using the Taguchi method / Vilhekar, Raman (Rights reserved)
  • Research on the impact of rain ingestion considering s-shaped inlet distortion on the performance of a centrifugal compressor / Wang, He (Rights reserved)
  • An integrated review of multiphysics issues and challenges in the design and implementation of gas turbine blades for jet engine applications / Pawar, Akash (Rights reserved)
  • Effect of Reynolds number variation on thermal performance and flow characteristics of heart pin fins in trailing edge / Goveraiahgari, Venkatesh (Rights reserved)
  • Investigation of flow and thermal behavior in multi-stage high-pressure compressor disk cavities / Li, Xiangyu (Rights reserved)
  • Analysis and improvement of negative pre-swirl recirculation casing treatment in a centrifugal compressor / Jin, Hong-ze (Rights reserved)
  • Effect of primary nozzle exit diameter on underexpanded coaxial jet characteristics / Bose Gurusamy, Chandra (Rights reserved)
  • Innovative modification of the NACA 0012 airfoil for enhanced lift and aerodynamic efficiency: CFD and experimental validation / Suresh, Sanoj P. (Rights reserved)
  • A high-dimensional and high-precision onboard modeling method for adaptive variable cycle engine / Zheng, Qiangang (Rights reserved)
  • Passive movement characteristics analysis and collision risk assessment of floating ring seals of aero-engine / Hu, Tingxun (Rights reserved)
  • A hybrid onboard model for aero-engine direct thrust predictive control / Zheng, Qiangang (Rights reserved)
  • Performance study of bypass dual throat nozzle based on numerical simulation / Liu, Xiaodong (Rights reserved)
  • A review of life cycle uncertainty factors and modeling methods for aero engine high-pressure compressor / Zhang, Jiaxuan (Rights reserved)
  • Frontmatter (Rights reserved)
  • Experimental investigation on the effect of non-circular ring tab on mixing characteristics of subsonic and underexpanded jets / Subramanian, Thanigaiarasu (Rights reserved)
  • Experimental study of jet-tab method with different tab lengths / Subramaniyan, Manikandan (Rights reserved)
  • Flow field characteristics of isolator with fluidic injection / Pinnam, Lovaraju (Rights reserved)
  • Computational study on heat transfer augmentation with pencil pin fins and ribbed surfaces in wedge channels / Goveraiahgari, Venkatesh (Rights reserved)
  • Turbojet module sizing for integration with turbine-based combined cycle engine / Subramanian, Rajashankar (Rights reserved)
  • Research on real-time improvement method of on-board physical mechanism model of turboshaft engine based on neural network / Liu, Yuan (Rights reserved)
  • A torsional vibration coupling dynamic modeling and analysis method for engine/power transmission systems in coaxial high-speed helicopters / Zhu, Shicheng (Rights reserved)
  • Numerical analysis of the sensitivity of combustion flow characteristics to key parameters in constricted cavity-jet combustor / Yan, Pinghua (Rights reserved)
  • Effect of forward swept blade on transonic high pressure ratio centrifugal compressor under different conditions / Tian, Boyu (Rights reserved)
  • Influence mechanism of advance ratio on the aerodynamic performance of a contra-rotating propfan / Zhiyuan, Cao (Rights reserved)
  • Effect of fin geometry on flow and heat transfer in wedge-shaped ducts: a numerical approach / Goveraiahgari, Venkatesh (Rights reserved)
  • Numerical investigation of the effect of self-excited sweeping jet actuator on flow separation in a compressor cascade / Shi, Yanchun (Rights reserved)
  • Numerical investigation of a novel mushroom-shaped cooling hole for enhanced film cooling performance / Boualem, Khadidja (Rights reserved)
  • Effects of Greitzer’s parameter and throttle valve coefficient on stall-surge transition in single-stage axial compressors / Meskine, Naima (Rights reserved)
  • Study on the relationship between radial flow and rotating instability characteristics under different axial clearances / Li, Hefei (Rights reserved)
  • Influence of creep on the modern single shaft gas turbine rotor blades durability / Smetankina, Natalia (Rights reserved)
  • Vibration suppression design for a turboshaft engine with shared bearing cavity structure / Li, Gaiqi (Rights reserved)
  • A physical-data-driven combined transfer learning method for gas turbine performance estimation / Ao, Ran (Rights reserved)
  • Optimization design method for accelerated control law of engine life extension considering combustion chamber outlet temperature distribution / Liu, Wei (Rights reserved)
  • Frontmatter (Rights reserved)
  • A method for evaluating the time-averaged and unsteady characteristics of flow loss in axial compressors / Huang, Yuhui (Rights reserved)
  • Research on adjoint-based customized integrated passage design of Rotor 67 / Li, Bowen (CC BY)
  • Investigation of the influence of an S-shaped isolator on the combustion characteristics of a supersonic combustion chamber / Yang, Zhiwei (Rights reserved)
  • Analysis of the dynamic characteristics of compliant foil gas seal with bearing-rotor system / Wang, Xueliang (Rights reserved)
  • Investigation on aerodynamic interference mechanism of a contra-rotating propfan under take-off condition / Zhiyuan, Cao (Rights reserved)
  • Enhancing fuel-air mixing and flame stability using double cavity with multiple struts scramjet propulsion / Roga, Sukanta (Rights reserved)
  • Integration of multi module flow domain to demonstrate the full engine aero-flow path simulation of Single Spool Turbojet Engine / Yogesh, Thuraganur V. (Rights reserved)
  • Uncertainty quantification by probabilistic analysis of Stirling engine performance / Gorla, Rama Subba Reddy (Rights reserved)
  • An energy method for dry friction damping of ring damper in labyrinth seal structure under radial vibration / Gao, Shimin (Rights reserved)
  • Impact of convex-side blade attachments on savonius vertical axis wind turbines performance at low wind speeds / Kumar, Yogesh (Rights reserved)
  • Deformation and fatigue life analysis of axial flow compressor blade based on fluid-structure interaction / Zhang, Xinzhe (Rights reserved)
  • Recent advancements in Scramjet combustor: technologies, fuel strategies, and performance challenges / Roga, Sukanta (Rights reserved)
  • Quantification of uncertainty propagation in transient heat transfer from flux-base extended surface / Gorla, Rama Subba Reddy (Rights reserved)
  • Impact of mass flow ratio on the aero-thermal performance of a film-cooled nozzle guide vane / Gudla, Babji (Rights reserved)
  • Uncertainty propagation in transient heat transfer from an extended surface / Gorla, Rama Subba Reddy (Rights reserved)
  • Uncertainty quantification of leakage characteristics of stepped labyrinth seals based on sparse PC-Kriging model / Xu, Decheng (Rights reserved)
  • Effects of splitter blade on vaned-diffuser stall and the corresponding warning method / Zhao, Jiayi (Rights reserved)
  • Minimum specific fuel consumption performance-seeking control for variable cycle engine based on CHOA-SQP hybrid algorithm and active disturbance rejection control / Fan, Tianfu (Rights reserved)
  • A novel degradation estimation of lifecycle health monitoring for aircraft engine gas path rotational components / Zou, Zelong (Rights reserved)
  • Frontmatter (Rights reserved)
  • Determination of the modern marine single shaft gas turbine rotor blades fatigue strength parameters / Smetankina, Natalia (Rights reserved)
  • Predicting compressor mass flow rate using various machine learning approaches / Yazar, Isil (Rights reserved)
  • Role of different cavity flame holders on the performance characteristics of supersonic combustor / Shajahan, Shaik (Rights reserved)
  • Simple model of turbine-based combined cycle propulsion system and smooth mode transition / Liu, Jun (Rights reserved)
  • Review of gliding arc plasma assisted ignition and combustion for gas turbine application / Gong, Ka (Rights reserved)
  • Performance analysis of a planar shaped strut injector based supersonic combustion chamber / Roga, Sukanta (Rights reserved)
  • Research on performance seeking control of turbofan engine in minimum hot spot temperature mode / Liu, Yabing (Rights reserved)
  • Performance evaluation of a scramjet engine utilizing varied cavity aft wall divergence with parallel injection in a reacting flow field / Maheswaran, Nagarathinam (Rights reserved)
  • Interaction effects between the rotor wake and hub leakage flow in a multi-stage cantilevered compressor / Deng, Hefang (Rights reserved)
  • Compensator based improved model predictive control for Aero-engine / Pang, Shuwei (Rights reserved)
  • Frontmatter (Rights reserved)
  • Flow pattern formation due to the interdependency of multi-component interactions and their impact on the performance of turbine and exhaust duct of gas turbine / Yogesh, Thuraganur V. (Rights reserved)
  • Speed controller design for turboshaft engine using a high-fidelity AeroThermal model / Yazar, Isil (Rights reserved)
  • Numerical and experimental study on the critical geometric variation based on sensitivity analysis on a compressor rotor / Wang, Yan (Rights reserved)
  • Numerical analysis of brush seal hysteresis based on orthogonal test method / Xiao, Furen (Rights reserved)
  • Constant temperature line identification on prototype gas turbine combustor with multi-colour change coating / Antony Raj, Gnana Sagaya Raj (Rights reserved)
  • Performance analysis of pulse detonation ramjet / Luo, Zhenkun (Rights reserved)
  • Sensitivity analysis of aero-engine performance optimization control system and its hardware test verification / Fang, Juan (Rights reserved)
  • Investigation on flow characteristics and its effect on heat transfer enhancement in a wedge channel with combination of circular, oblong, teardrop, and pencil pin fins / Venkatesh, Goveraiahgari (Rights reserved)
  • Study of vortex throttle characteristics with adjustable resistance by rotation of the vortex chamber inlet channel / Levitsky, Inna (Rights reserved)
  • Frontmatter (Rights reserved)
  • Conjugated heat transfer characteristics of ribbed-swirl cooling in turbine blade under rotation condition / Xiao, Kun (Rights reserved)
  • Deep residual ensemble model for predicting remaining useful life of turbo fan engines / Selvaraj, Sharanya (Rights reserved)
  • Effect of inlet diameter on the flow structure and performance for aluminum-based water-jet engine / Xu, Wei (Rights reserved)
  • Aero-engine direct thrust control based on nonlinear model predictive control with composite predictive model / Chen, Haoyang (Rights reserved)
  • Performance analysis of a gas turbine engine with intercooling and regeneration process - Part 1 / Quadros, Jaimon D. (Rights reserved)
  • Computational analysis of the scramjet mode of the RBCC inlet using micro vortex generators / Raj, Ritul (Rights reserved)
  • Ignition experimental study based on rotating gliding arc / Peng, Ting (Rights reserved)
  • Upgraded one-dimensional code for the design of a micro gas turbine mixed flow compressor stage with various crossover diffuser configurations / van Eck, Hano (Rights reserved)
  • Thermal performance of teardrop pin fins and zig zag ribs in a wedge channel / Venkatesh, Goveraiahgari (Rights reserved)
  • Experimental study on flow field and combustion characteristics of V-gutter and integrated flameholders / Li, Jie (Rights reserved)
  • ˜Theœ study of cascading effect in the integration of intake with gas turbine engine bay in subsonic cruise vehicle / Yogesh, Thuraganur V. (Rights reserved)
  • Application of KH-RT model in lifting flame of methanol jet atomization / Wang, Qiuyin (Rights reserved)
  • Enhancing transonic compressor rotor efficiency by flow analysis-driven blade section modification / Shi, Hengtao (Rights reserved)
  • Effect of perforated wall in controlling the separation due to SWBLI at Mach no. 5 to 9 / Babu R, Dinesh (Rights reserved)
  • Flight trajectory optimization study of a variable-cycle turbine-based combined cycle engine hypersonic vehicle based on airframe/engine integration / Fu, Yu (Rights reserved)
  • Multi-objective optimization of the aerodynamic performance of butterfly-shaped film cooling holes in rocket thrust chamber / Yu, Ningning (Rights reserved)
  • Probabilistic analysis of blade flutter based on particle swarm optimization-deep extremum neural network / Wei, Jingshan (Rights reserved)
  • Multi-nozzle thrust matching control of STOVL engine / Pang, Shuwei (Rights reserved)
  • Investigation of varying tip clearance gap and operating conditions on the fulfilment of low-speed axial flow fan / Vala, Jignesh R. (Rights reserved)
  • Impact of annular ribs in sudden expansion flow conditions to control base pressure / Kengaiah, Vijayaraja (Rights reserved)
  • Research on vibration damping of integral squeeze film damper based on fan rotor tester of turbofan / Zhu, Gang (Rights reserved)
  • Exploration of shock-induced flow dynamics and turbulence-driven combustion optimization in advanced cavity configurations of hydrogen fueled scramjet combustors / Shajahan, Shaik (Rights reserved)
  • Hypersonic boundary layer flow at an axisymmetric stagnation point on a blunt body / Kumari, Mahesh (Rights reserved)
  • Numerical analysis of pollutant formation and exhaust emission in a short annular combustor under part load operation / Mishra, Ranjan K. (Rights reserved)
  • Effect of preheated swirling multi-annular jets on mixing and flow characteristics in various expanded confinements / Srivastava, Ritesh (Rights reserved)
  • Frontmatter (Rights reserved)
  • A part-load performance analysis method for gas turbines based on the stage by stages model of the power turbine / Deng, Liping (Rights reserved)
  • Effect of lip-thickness on rectangular nozzle co-flowing subsonic jet / Gopalakrishnan, Ezhilmaran (Rights reserved)
  • Design optimization of a fluidic thrust vectoring system based on coanda effect using meta-models / Kara, Emre (Rights reserved)
  • Investigations of modified cooling hole injection angle configurations for improved trench film cooling performance / Vasudevan Girija, Krishna Anand (Rights reserved)
  • Analysis of leakage characteristics and structural optimization of two-stage floating ring seal / Hu, Tingxun (Rights reserved)
  • Influence of conical shaft stiffness on the dynamic characteristics of flexible rotor / Shi, Chenglong (Rights reserved)
  • Numerical simulations of a turbulent lifted hydrogen flame in vitiated coflow with flamelet generated manifold approach / Lai, Zhengxin (Rights reserved)
  • Multi-parameter study on array-jets impingement with crossflow temperature effect / He, Juan (Rights reserved)
  • Numerical study of effect of the casing slot on the tip leakage vortex and vortex cavitation of a fuel pump / Zhang, Ting (Rights reserved)
  • A novel design methodology for preventing dislocation in the Zig-zag shroud / Du, Chenhong (Rights reserved)
  • Simulation and analysis of the over-expanded flow field in asymmetric nozzles with lateral expansion / Wang, Zhenghe (Rights reserved)
  • Influence of non-axisymmetric endwall profiling under incoming vortex on the corner separation of a diffusion cascade / Zhang, Ting (Rights reserved)
  • Optimization of labyrinth seal leakage with independently varied tooth parameters using efficient global optimization / Xu, Decheng (Rights reserved)
  • Numerical investigation of force over the horizontal jet tab of various sector angle fixed to the convergent-divergent nozzle exit / Ahmed, Asad R. (Rights reserved)
  • Effects of bleed pressure on shock-wave/boundary-layer interactions in a transonic compressor stator with suction holes / Li, Bai (Rights reserved)
  • Parametric analysis of thermal cycle of a short take-off and vertical landing engine / Mo, Zhihan (Rights reserved)
  • Improving thermal performance of turbine blade with combination of circular and oblong fins in a wedge channel: a numerical investigation / Venkatesh, Goveraiahgari (Rights reserved)
  • Frontmatter (Rights reserved)
  • Frontmatter (Rights reserved)
  • Research on an optimization design method for a TBCC propulsion scheme / Wu, Pinxin (Rights reserved)
  • Research on the design method of mode transition control law for Ma6 external parallel TBCC engine / Jiao, Guiqian (Rights reserved)
  • Influence of metal magnesium addition on detonation initiation in shock wave focusing Pulse Detonation Engine / Wu, Yun-Kai (Rights reserved)
  • Investigation on effect of injector orifice diameter on injector atomization and combustion characteristics of pulse detonation combustor / Ding-Ding, Wang (Rights reserved)
  • Performance analysis of a gas turbine engine via intercooling and regeneration- Part 2 / Poojary, Suhas (Rights reserved)
  • Frontmatter (Rights reserved)
  • Conjugate heat transfer analysis on double-wall cooling configuration including jets impingement and film holes with conformal pins / Chen, Chenlin (Rights reserved)
  • Numerical study on aerodynamic performance of an intake duct affected by ground effect / Shi, Yalin (Rights reserved)
  • Numerical investigation on mixing of heated confined swirling coaxial jets with blockage / Srivastava, Ritesh (Rights reserved)
  • Effect of asymmetric leading edge on transition of suction side / Chen, Yutian (Rights reserved)
  • A new schedule method for compact propulsion system model / Bai, Yu (Rights reserved)
  • Probabilistic analysis of solid oxide fuel-cell integrated with gas turbine / Gorla, Rama Subba Reddy (Rights reserved)
  • Frontmatter (Rights reserved)
  • Air tab location effect on supersonic jet mixing / Govindan, Mahendra Perumal (Rights reserved)
  • Finite element based dynamic analysis of a porous exponentially graded shaft system subjected to thermal gradients / Vaka, Vijayakumar (Rights reserved)
  • Thrust-matching and optimization design of turbine-based combined cycle engine with trajectory optimization / Zhu, JianFeng (Rights reserved)
  • Frontmatter (Rights reserved)
  • Experimental and numerical investigations on controlled parameter selection methods for kerosene-fueled scramjet / Jiao, Guiqian (Rights reserved)
  • Design and analysis of air intake of subsonic cruise vehicle with experimental validation / T. V., Yogesh (Rights reserved)
  • ˜Theœ overall film cooling performance of crescent holes / Wang, Qiuyin (Rights reserved)
  • Research on cascade control method for turboshaft engine with variable rotor speed / Yao, WenRong (Rights reserved)

E-Pflicht Kooperationsprojekt "NP Regional"

Diese Publikation wurde im Rahmen des Kooperationsprojekts "NP Regional" von der Deutschen Nationalbibliothek übernommen. Sie fällt unter die E-Pflicht (Elektronische Pflichtpublikationen in Berlin).

Downloads

Downloads

Full record

TOC

Image fragment

Link to the viewer page with highlighted frame Link to IIIF image fragment

Formats and links

Cite

Cite

The following citation links are available for the entire work or the page displayed:

Full record

Citation recommendation

Please check the citation before using it.

Contact

Have you found an error? Do you have any suggestions for making our service even better or any other questions about this page? Please write to us and we'll make sure we get back to you.

What is the first letter of the word "tree"?:

I hereby confirm the use of my personal data within the context of the enquiry made.