Performance Sensitivities of Rotating Detonation Engines Installed onto Waverider Forebodies-Reference-Cited by-同舟云学术

Performance Sensitivities of Rotating Detonation Engines Installed onto Waverider Forebodies

Published:2019-03 Issue:2 Volume:35 Page:289-302
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Mizener Andrew R.¹,Lu Frank K.¹,Rodi Patrick E.²

Affiliation:

1. University of Texas at Arlington, Arlington, Texas 76019

2. Lockheed Martin Corporation, Houston, Texas 77258

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B37033

Reference60 articles.

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2. HenryJ. R.AndersonG. Y. “Design Considerations for the Airframe-Integrated Scramjet,” NASA TM-X-2895, 1973.

3. KumarA. J. “Numerical Simulations of Scramjet Inlet Flow Fields,” NASA TP-2517, 1986.

4. Scramjet Engines: The First Forty Years

5. EggersA. J.ResknioffM. M.DennisD. H. “Bodies of Revolution Having Minimum Drag at High Supersonic Airspeeds,” NASA TR-1306, 1957.

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