Reduced-order-modeling of the transient starting in supersonic passages

Author:

Inhestern Lukas BenjaminORCID,Peitsch Dieter,Paniagua GuillermoORCID

Funder

H2020 Marie Skłodowska-Curie Actions

European Commission

U.S. Department of Energy

Horizon 2020

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference47 articles.

1. Preliminary investigation of supersonic diffusers;Kantrowitz,1945

2. The formation and stability of normal shock waves in channel flows;Kantrowitz,1947

3. A. Karanian, C. Kepler, Experimental hypersonic inlet investigation with application to dual-mode scramjet, in: Propulsion Joint Specialist Conference, p. 588.

4. Starting phenomena for hypersonic inlets with thick turbulent boundary layers at Mach 6;Goldberg;Natl. Aeronaut. Space Adm.,1971

5. Effect of cooling of the central body on the start-up separation of the flow at the intake and the throttling characteristics of air scoops at supersonic and hypersonic velocities;Gurylev;Fluid Mech. Sov. Res.,1978

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