Semiempirical method of calculating overexpanded turbulent separated flow in a conical laval nozzle-Reference-Cited by-同舟云学术

Semiempirical method of calculating overexpanded turbulent separated flow in a conical laval nozzle

Published:1989 Issue:6 Volume:23 Page:851-856
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Malik T. I.,Tagirov R. K.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/BF01051818.pdf

Reference15 articles.

1. G. I. Petrov, V. Ya. Likhushin, I. P. Nekrasov, and L. I. Sorkin, ?Effect of viscosity on supersonic flow with shocks,? Tr. TsIAM, No. 22, 28 (1952).

2. M. V. Herbert and R. J. Herd, ?Boundary-layer separation in supersonic propelling nozzles,? Aeronaut. Res. Council Rep. Mem., No. 3421, 71 (1964).

3. H. L. G. Sunley and V. N. Ferriman, ?Jet separation in conical nozzles,? J. R. Aeronaut. Soc.,68, 808 (1964).

4. O. S. Zelenkov and A. V. Yurkov, ?Experimental investigation of flow separation in underexpanded conical nozzles,? Uch. Zap. Leningr. Gos. Univ. Ser. Mat. Nauk, Issue 43, No. 338, 94 (1968).

5. A. P. Vasil'ev, V. M. Kudryavtsev, V. A. Kuznetsov, et al., Fundamentals of the Theory and Design of Liquid-Fueled Rocket Engines [in Russian], Vyssh. Shkola, Moscow (1975).

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical study of ways to prevent side loads in an over–expanded rocket nozzles during the launch stage;Acta Astronautica;2019-10

2. Quasi-one-dimensional modeling of pressure effects in supersonic nozzles;Aerospace Science and Technology;2017-11

3. Evaluation of Quasi-One-Dimensional Modeling for Nozzle Flow Separation;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23

4. Numerical simulation of fluidic thrust vectoring in an axisymmetric supersonic nozzle;Journal of Mechanical Science and Technology;2014-12

5. A study on the thrust vector control using a bypass flow passage;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2014-11-13