Experimental Investigation of Nozzle/Plume Aerodynamics at Hypersonic Speeds PDF Download

Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723048074
Category :
Languages : en
Pages : 152

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Book Description
The 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. Heinemann, K. and Bogdanoff, David W. and Cambier, Jean-Luc Unspecified Center AERODYNAMICS; COMBUSTION CHAMBERS; COMPUTATIONAL FLUID DYNAMICS; DETONATION WAVES; HYDROGEN FUELS; HYPERSONIC SPEED; SHOCK LAYERS; SHOCK TUNNELS; UNSTEADY FLOW; CALIBRATING; COMPUTERIZED SIMULATION; FUEL SYSTEMS; HIGH TEMPERATURE; TEST CHAMBERS; WEDGES...