Methods for determining the internal thrust of scramjet engine modules from experimental data-Reference-Cited by-同舟云学术

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Methods for determining the internal thrust of scramjet engine modules from experimental data

Published:1990-07-16 Issue: Volume: Page:
ISSN:
Container-title:26th Joint Propulsion Conference
language:
Short-container-title:

Author:

VOLAND RANDALL¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-2340

Reference24 articles.

1. Jilly. L. F., Editor: Hypesonic Research Engine Project-Phase 11, Aerothermodynamic Integration Model Development, Final Technical Report. NASA Contract No. NAS1-6666. Document No. AP-75-11133.

2. Burnette, T. D.: Dual Mode Scramjet-Part 111, Engine Design and Performance Characteristics. The Marquardt Corporation, Technical Report AFAPL-TR-67-132,Part111,June 1968.

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. Recent advances and prospects in hypersonic inlet design and intelligent optimization;Aerospace Science and Technology;2024-03

2. Three-Component Force Measurements for Scramjet Engines 1) Engine Drag from Mach 4 to Mach 8 Flight Conditions;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

3. Force Measurements of Fixed-Geometry Scramjet Engines from Mach 4 to 8 Flight Conditions;AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference;2002-06-26

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