Comparison of a Direct-Connect and Freejet Dual-Mode Scramjet-Reference-Cited by-同舟云学术

Comparison of a Direct-Connect and Freejet Dual-Mode Scramjet

Published:2015-09 Issue:5 Volume:31 Page:1380-1392
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Steva Thomas B.¹,Goyne Christopher P.¹,Rockwell Robert D.¹,Cresci Daniel²,Osborne Jonathan W.³

Affiliation:

1. Department of Mechanical and Aerospace Engineering, University of Virginia, Charlottesville, Virginia 22904

2. Alliant Techsystems Operations LLC (Orbital ATK), Ronkonkoma, New York 11779

3. MIRA Facilities Management, LLC, Arnold Air Force Base, Tennessee 37389

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35221

Reference25 articles.

1. HeiserW. H.PrattD. T., Hypersonic Airbreathing Propulsion, AIAA Education Series, AIAA, Washington, D.C., 1994, pp. 528–537.

2. Expansion of the scramjet ground test envelope of the Hypulse facility

3. EmamiS.TrexlerC. A.AuslenderA. H.WeidnerJ. P. “Experimental Investigation of Inlet-Combustor Isolators for a Dual-Mode Scramjet at a Mach Number of 4,” NASA TP-3502, May 1995.

4. Behavior of shock trains in a hypersonic inlet/isolator model with complex background waves

5. The Art of Extracting One-Dimensional Flow Properties from Multi-Dimensional Data Sets

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