Unsteady effects of a hypersonic type IV shock interaction

Author:

Lind Charles1,Lewis Mark1

Affiliation:

1. Maryland, Univ., College Park

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. III t.lie Prscncrof an Iinpingiiig Shock," Arroii;itit,ical Research Instit.utr, of Swedrn, FAA fkport, I IT, 1968.

2. 3Holdm,M. S., Wict.iiig. A. It., Mosdli.I. H.mil Class, (, "Studies of Aerotlierriial 1,oads Gciirratrd in Rrgions of Shoc.k/Shock Intcrartioiiiii Ilypersonic Flow," AlAA 88-0477,Jaiioary 19x8.

3. sI'ralilii,R. K.>Stewart,J. It., aiid Tliar?jiL, I(.It. "Shock Interf(vtwcr Stiidim nii it (:irciilar (`yliiidrr at, Mach IC," AlAA I'npr90-0(i06,liiiiiiiryl 991J.

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2. Influence of Blunting Manner of the Lip Highlight of Hypersonic Inlet on the Aerothermodynamic Performance;17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2011-04-11

3. Shock Interaction Control for Scramjet Cowl Leading Edges;AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference;2005-05-16

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5. Shock/shock interaction experiments in the High Enthalpy Shock Tunnel Goettingen;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12

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