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Strip blowing from a wedge at hypersonic speeds

Messiter, Arthur F.
Matarrese, M. D.

Publication date

January 1995

DOI

10.2514/3.12372

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

ISSN

0001-1452

Journal

AIAA Journal

Language

English

Citation count (estimate)

3

Abstract

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76052/1/AIAA-12372-854.pd

Extracted data

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Edwards, C. L. W.
Anders, J. B.

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Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer se...

On quasi-steady boundary-layer separation in supersonic flow. Part 2. Downstream moving separation point

Ruban, A
Djehizian, A
Kirsten, J
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In this paper we study the perturbations produced in the boundary layer by an impinging oblique shoc...

Separation over a flat plate-wedge configuration at oceanic Reynolds numbers

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May 1973

An experimental study of flow over a two-dimensional flat plate-wedge configuration is presented. Th...

Strip blowing from a wedge at hypersonic speeds

Messiter, Arthur F.
Adamson, Thomas Charles Jr.

January 1991

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76964/1/AIAA-1991-32-677.pd

Control of hypersonic aerodynamic forces with surface blowing

Messiter, Arthur F.
Adamson, Thomas Charles Jr.
Matarrese, M. D.

January 1991

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76211/1/AIAA-10846-311.pd

Control of hypersonic aerodynamic forces with surface blowing.

Matarrese, Michael David

January 1993

Aerodynamic forces are obtained for laminar flow past a slender wedge at high Mach number and high R...

Effect of contact surface bluntness on massive blowing from a wedge in hypersonic flow /

Emanuel, George, author.
United States. Air Force. Systems Command. Space Systems Division, issuing body.
Aerospace Corporation, sponsor.

An inviscid, compressible analysis is given for massive blowing from the porous surface of a wedge o...

Blowing from a porous cone or wedge when the contact surface is straight /

Emanuel, George, author.
United States. Air Force. Systems Command. Space Systems Division, issuing body.
Aerospace Corporation, sponsor.

An analysis of inviscid, compressible flow over a porous conne or wedge is given where the body is i...

A numerical study of hypersonic flow with strong surface blowing.

Carter, Nelson David

January 1992

A possible means of controlling hypervelocity vehicles within the atmosphere is the use of boundary-...

Drag estimation on wedge-shaped protuberances in high-speed flows

Kshitij, Abhinav
Prince, Simon A.
Stollery, John L.

January 2020

A semi-empirical method is developed to estimate drag on wedge-shaped projections in hypersonic flow...

A study of flow separation in regions of shock wave-boundary layer interaction in hypersonic flow /

Holden, Michael S., author.
Aerospace Research Laboratories (U.S.), issuing body.
New York University. Aerospace and Energetics Laboratory, sponsor.

This report describes a theoretical and experimental investigation of the properties of attached and...

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Volkov, Konstantin

December 2022

The development of the flow pattern that arises during the interaction of a shock wave with a wedge ...

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Carter, Nelson
Van Leer, Bram

January 1990

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76476/1/AIAA-1990-603-194.pd

A real-gas study of low-density wedge-induced laminar separation on a highly cooled blunt flat plate at M infinity equals 12

Anders, J. B.
Edwards, C. L. W.

March 1968

Real gas wedge-induced laminar separation on cooled blunt flat plate at hypersonic spee

Experimental Investigations of Leading Edge Bluntness in Shock Boundary Layer Interactions at Hypersonic Speeds

Lakshman, Srinath

January 2015

Shock Boundary Layer Interactions (SBLIs) and shock-shock interactions are some of the most fundamen...

Low-density, leading-edge bluntness, and ablation effects on wedge-induced laminar boundary layer separation at moderate enthalpies in hypersonic flow

Edwards, C. L. W.
Anders, J. B.

October 1968

Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer se...

On quasi-steady boundary-layer separation in supersonic flow. Part 2. Downstream moving separation point

Ruban, A
Djehizian, A
Kirsten, J
Kravtsova, MA

June 2020

In this paper we study the perturbations produced in the boundary layer by an impinging oblique shoc...

Separation over a flat plate-wedge configuration at oceanic Reynolds numbers

Campbell, D. R.

May 1973

An experimental study of flow over a two-dimensional flat plate-wedge configuration is presented. Th...