Mach 4 Test Results of a Dual-Flowpath, Turbine Based Combined Cycle Inlet-Reference-Cited by-同舟云学术

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Mach 4 Test Results of a Dual-Flowpath, Turbine Based Combined Cycle Inlet

Published:2006-06-15 Issue: Volume: Page:
ISSN:
Container-title:14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Albertson Cindy¹,Emami Saied¹,Trexler Carl¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-8138

Reference8 articles.

1. Unsteady pressure behavior in a ramjet/scramjet inlet

2. NASA hypersonic flight demonstrators—overview, status, and future plans

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3. On incident shock wave/boundary layer interactions under the influence of expansion corner;Journal of Fluid Mechanics;2024-06-03

4. Design Procedure of a Variable Rectangular Inlet for TBCC Engine Considering Mass Flow Requirements;International Journal of Aeronautical and Space Sciences;2024-04-22

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