Effects of nonuniform Mach-number entrance on scramjet nozzle flowfield and performance-Reference-Cited by-同舟云学术

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Effects of nonuniform Mach-number entrance on scramjet nozzle flowfield and performance

Published:2016-12 Issue: Volume:129 Page:201-210
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Zhang Pu,Xu Jinglei,Quan Zhibin,Mo Jianwei

Funder

NSFC

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Strategy for developing air-breathing aerospace planes;Mehta;J. Aircr.,1996

2. Studies of scramjet/airframe integration techniques for hypersonic aircraft;Edwards;AIAA Pap.,1975

3. Experimental results for a hypersonic nozzle/afterbody flow field;Spaid;AIAA Pap.,1992

4. Scramjet propulsion;Curran;AIAA: Prog. Astronaut. Aeronaut.,2000

5. Propulsion aspects of hypersonic turbo-ramjet-engines with special emphasis on nozzle/afterbody intergration;Herrman;ASME Pap.,1991

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4. Validation for Aerodynamic Performance on Over-Expanded State of Single Expansion Ramp Nozzle Configuration;Aerospace;2022-11-14

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