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Experimental Investigation of Nozzle/Plume Aerodynamics at Hypersonic SpeedsThe work performed by D. W. Bogdanoff and J.-L. Cambier during the period of 1 Feb. - 31 Oct. 1992 is presented. The following topics are discussed: (1) improvement in the operation of the facility; (2) the wedge model; (3) calibration of the new test section; (4) combustor model; (5) hydrogen fuel system for combustor model; (6) three inch calibration/development tunnel; (7) shock tunnel unsteady flow; (8) pulse detonation wave engine; (9) DCAF flow simulation; (10) high temperature shock layer simulation; and (11) the one dimensional Godunov CFD code.
Document ID
19930008896
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Heinemann, K. (Eloret Corp. Sunnyvale, CA, United States)
Bogdanoff, David W. (Eloret Corp. Sunnyvale, CA, United States)
Cambier, Jean-Luc (Eloret Corp. Sunnyvale, CA., United States)
Date Acquired
September 6, 2013
Publication Date
December 3, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-191368
NAS 1.26:191368
Report Number: NASA-CR-191368
Report Number: NAS 1.26:191368
Accession Number
93N18085
Funding Number(s)
CONTRACT_GRANT: NCC2-487
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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