Effects of Mach Number on the Performance of a Diverterless Supersonic Inlet
Author:
Affiliation:
1. Sharif University of Technology, 11365 Tehran, Iran
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference24 articles.
1. Elements of Propulsion: Gas Turbines and Rockets
2. Buzz Cycle Description in an Axisymmetric Mixed-Compression Air Intake
3. Intake Aerodynamics, Second Edition
4. Effects of Shock Wave/Boundary-Layer Interaction on Performance and Stability of a Mixed-Compression Inlet
5. GoldsmithE. L.SeddonJ., Practical Intake Aerodynamic Design, 2nd ed., AIAA Education Series, AIAA, Washington, D.C., 1993, pp. 320–392.
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