Numerical Simulation on Ramjet Inlet with Different Cowl Leading Edge-Reference-Cited by-同舟云学术

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Numerical Simulation on Ramjet Inlet with Different Cowl Leading Edge

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:35th AIAA Fluid Dynamics Conference and Exhibit
language:
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Author:

Chen Xiong¹,Zheng Ya¹,Zhou Changsheng¹,Ju Yutao¹

Affiliation:

1. Nanjing University of Science and Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-5288

Reference24 articles.

1. Computational Investigation of a Method to Compress Air Fluidically in Supersonic Inlets

2. Angeles, California.,Jun.,1999.

3. supersonicinlets,"JournalofSpacecraftandRockets,Vol.38, No.1, 2001, pp.51-59.

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1. A Trend Analysis and Future Opportunities on the Solid Fuel Ramjet Technology;Journal of the Korean Society of Propulsion Engineers;2024-06-30

2. RAMJET PROPULSION FOR PROJECTILES-AN OVERVIEW OF WORLDWIDE ACHIEVEMENTS AND FUTURE OPPORTUNITIES;International Journal of Energetic Materials and Chemical Propulsion;2022

3. Numerical Simulation on Aerodynamics of Ramjet Projectiles;Advanced Materials Research;2011-02

4. Experimental and Numerical Research on Inlet of Ramjet Assisted Range Projectile;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

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