Experimental investigation of start/unstart process during hypersonic intake at Mach 6 and its control-Reference-Cited by-同舟云学术

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Experimental investigation of start/unstart process during hypersonic intake at Mach 6 and its control

Published:2021-06 Issue: Volume:113 Page:106688
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Saravanan R.,Desikan S.L.N.,Francise K.J.,Kalimuthu R.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference76 articles.

1. Scramjets integrate air and space;Andreadis;Ind. Phys.,2004

2. How much compression should a scramjet inlet do?;Smart;AIAA J.,2012

3. Hypersonic Air Breathing Propulsion;Heiser,1994

4. Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6;Holland,1994

5. D.M. Van Wie, F.T. Kwok, R.F. Walsh, Starting characteristics of supersonic inlets, AIAA Paper 1996–2914.

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