Some Flow-Structure Features of Scramjet Isolator

Author:

Shang Joseph1

Affiliation:

1. Mechanical and Materials Engineering Department, Wright State University

Publisher

American Institute of Aeronautics and Astronautics

Reference23 articles.

1. Ferri,A., ReviewofProblems inApplicationofSupersonic Combustion,J. RoyalAeronauticalSoc.,Vol. 68,No.645,1964,pp.575-597.

2. Murthy,S.N.B. and Curran, E.T.,HighSpeed FlightPropulsionSystems, Progress inAeronautics and Astronautics,AIAA,1991.

3. Curran, E.T.,Heiser,W.H.,Pratt,D.T., Fluid Phenomena in ScramjetCombustion Systems, Ann.Rev. Fluid Mech.,Vol.28,1996,pp.323-60.

4. Kurth, G., Critical Physical Phenomena inScramjet Propulsion,AGARD-CP-600,2002,pp. C5.1- C5.11.

5. Scramjet Engines: The First Forty Years

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1. Effects of boundary‐layers bleeding on performance parameters of hypersonic inlets;Aircraft Engineering and Aerospace Technology;2009-05-15

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