Scaling Effects on Side Load Generation in Subscale Rocket Nozzles

Author:

Stark Ralf H.,Genin Chloe

Publisher

American Institute of Aeronautics and Astronautics

Reference24 articles.

1. Experimental study of boundary layer separation in truncated ideal contour nozzles

2. Appearance of Restricted Shock Separation in Rocket Nozzles

3. Side-Load Phenomena in Highly Overexpanded Rocket Nozzles

4. 5Lawrence, R. A., Symmetrical and Unsymmetrical Flow Separation in Supersonic Nozzles, NASA CR 92587, Ph.D. Thesis,Institute of Technology of Southern Methodist University, Dallas, Texas, April5th,1967.

Cited by 3 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. Semi-empirical calibration of remote microphone probes using Bayesian inference;Journal of Sound and Vibration;2024-03

2. Analysis of the Aspiration Drag in Dual-Bell Nozzles;International Journal of Aeronautical and Space Sciences;2022-11-01

3. Supersonic Several Bells Design of Minimum Length Nozzle Contours for More Altitudes Level Adaptations;Arabian Journal for Science and Engineering;2021-05-27

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