Drag reduction characteristics of recirculation flow at rocket base in an RBCC engine under ramjet/scramjet mode-Reference-Cited by-同舟云学术

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Drag reduction characteristics of recirculation flow at rocket base in an RBCC engine under ramjet/scramjet mode

Published:2023-12 Issue: Volume: Page:
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

LI Menglei,SUN Mingbo,LI Peibo,YANG Daoning,AN Bin,YAO Yizhi,CHEN Jikai,WANG Taiyu,WANG Jiaoru

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference40 articles.

1. Combined rocket and airbreathing propulsion systems for space-launch applications;Daines;J Propuls Power,1998

2. Research progress of rocket based combined cycle engines;Wang;J Astronaut,2019

3. Rocket-based combined cycle propulsion system testing;Perkins;J Propuls Power,1998

4. Strutjet engine performance;Campbell;J Propuls Power,2001

5. Hueter U. Rocket-based combined cycle propulsion technology for access-to-space applications. Reston: AIAA; 1999. Report No.: AIAA-1999-4925.

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