Three-Component Force Measurements for Scramjet Engines 2) Effects of External Flow and Boundary Layer Ingestion

Author:

Mitani Tohru,Tarukawa Yuichi,Izumikawa Muneo,Watanabe Syuichi,Shimura Takashi

Publisher

Japan Society for Aeronautical and Space Sciences

Reference4 articles.

1. Thrust, Lift, and Pitching Moment of a Scramjet Engine

2. 2) Volluz, R. J.: Handbook of Supersonic Aerodynamics, Wind Tunnel Instrumentation and Operation, NAVORD Report 1488 (Vol. 6), 1961.

3. Three-Component Force Measurements for Scramjet Engines 1) Engine Drag from Mach 4 to Mach 8 Flight Conditions

4. 4) Trexler, C. A. and Souders, S. W.: Design and Performance at a Local Mach Number of 6 of an Integrated Scramejt Concept, NASA, TN D-7944, 1975.

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1. Aerodynamic Tests of Scramjet Engines with Variable Mach Number Nozzle;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2005

2. Evaluation of Air Capture Ratio of Scramjet Inlet by Multi-Point Pressure Measurement;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2005

3. Visualization and CFD Analysis around Hypersonic Space Plane;Transaction of the Visualization Society of Japan;2005

4. 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

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