Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle View on Open Library

Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle

by Oktay Baysal

No reviews yet
First published: 1992 1 language
Subjects
Afterbodies Hypersonic Aerodynamics Hypersonic nozzles

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by Oktay Baysal

Navier-Stokes calculations of transonic flows past cavities

Navier-Stokes calculations of transonic ...

Efficient gradient-based shape optimization methodology using inviscid/viscous CFD

Efficient gradient-based shape optimizat...

Navier-Stokes analysis of cold scramjet-afterbody flows

Navier-Stokes analysis of cold scramjet-...

Navier-Stokes calculations of scramjet-nozzle-afterbody flowfields

Navier-Stokes calculations of scramjet-n...

Aerodynamic design optimization with sensitivity analysis and computational fluid dynamics

Aerodynamic design optimization with sen...

Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization

Domain decomposition for aerodynamic and...

You Might Also Like

More in Afterbodies
Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds

Comparison of wind tunnel and flight tes...

Jack Nugent
Experimental aerothermodynamic research of hypersonic aircraft

Experimental aerothermodynamic research ...

Joseph W. Cleary
Validation of the NPARC code for nozzle afterbody flows at transonic speeds

Validation of the NPARC code for nozzle ...

James R. DeBonis
Wind-tunnel development of an SR-71 aerospike rocket flight test configuration

Wind-tunnel development of an SR-71 aero...

Computational design aspects of a NASP nozzle/afterbody experiment

Computational design aspects of a NASP n...

Stephen M. Ruffin
The effect of exhaust plume/afterbody interaction on installed scramjet performance

The effect of exhaust plume/afterbody in...

Thomas A. Edwards