Simultaneous measurement of aerodynamic and heat transfer data for large angle blunt cones in hypersonic shock tunnel

Author:

Sahoo Niranjan,Saravanan S.,Jagadeesh G.,Reddy K. P. J.

Publisher

Springer Science and Business Media LLC

Subject

Multidisciplinary

Reference31 articles.

1. Abdel-Jawad M M, Mee D J, Morgan R G, Jacobs, P A, Philpot J A 2001 Transient force measurements at superorbital speeds.Proc. 23rd Int. Symp. on Shock Waves (ed.) F K Lu, Fort Worth, TX, pp. 515–521

2. Alan P, Kennith L G 1965High-speed wind tunnel testing (New York: John Wiley & Sons)

3. Series in Aeronautical and Aerospace Engineering;J D Anderson,1989

4. Brian R H, John N P 1997 High enthalpy aerothermodynamics of a Mars entry vehicle Part 1: Experimental results,J. Spacecr. Rockets 34: 449–456

5. Cook W J, Felderman E J 1966 Reduction of data from thin film heat transfer gauge: A concise numerical technique.AIAA J. 4: 561–562

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