Over-under nozzle CFD study and comparison with data

Author:

Chang Ing1,Hunter Louis2

Affiliation:

1. Praire View A & M, TX

2. Lockheed Fort Worth Co., TX

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. Concepts for Advanced Airbreathing Propulsion Systems", Wright Labs Report WP-TR-92-3073,1991. (2) Hansen, P. "Cold Flow Model Tests to

2. and Wall Layer Model for Compressible Flows", AIAA 90-1483. v (5) Chien, K.Y. "Predictions of Channel

3. Predictions of Channel and Boundary-Layer Flows with a Low-Reynolds-Number Turbulence Model

Cited by 4 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. Fluid–structure interaction study of the splitter plate in a TBCC exhaust system during mode transition phase;Acta Astronautica;2015-07

2. Design and Experimental Study of an Over-Under TBCC Exhaust System;Journal of Engineering for Gas Turbines and Power;2013-10-21

3. HPC CHSSI CFD-7 - Scalable WIND from the NPARC Alliance;30th Plasmadynamic and Lasers Conference;1999-06-28

4. The NPARC Alliance - A progress report;33rd Joint Propulsion Conference and Exhibit;1997-07-06

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