Supersonic Boundary Layers

93 books
On supersonic-inlet boundary-layer bleed flowG. J. Harloff

On supersonic-inlet boundary-layer bleed flow

G. J. Harloff

1995No page data
Numerical simulation of shock/turbulent boundary layer interactionSedat Biringen

Numerical simulation of shock/turbulent boundary layer interaction

Sedat Biringen

1993No page data
Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experimentLaurie A. Marshall
⏱ 48m

Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment

Laurie A. Marshall

199948 pp.
Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interactionAerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)

Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction

Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)

1994No page data
Boundary layer measurements at supersonic nozzle throatsMerwin Sibulkin
⏱ 26m

Boundary layer measurements at supersonic nozzle throats

Merwin Sibulkin

195626 pp.
Flow characteristics in boundary layer bleed slots with plenumA. Hamed

Flow characteristics in boundary layer bleed slots with plenum

A. Hamed

1995No page data
Supersonic laminar boundary layers on conesJohn Caister Cooke
⏱ 25m

Supersonic laminar boundary layers on cones

John Caister Cooke

196925 pp.
Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flowsNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
⏱ 4h 58m

Special course on shock-wave/boundary-layer interactions in supersonic and hypersonic flows

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1993298 pp.
Boundary-layer separation in supersonic propelling nozzlesHerbert, M. V.
⏱ 1h 11m

Boundary-layer separation in supersonic propelling nozzles

Herbert, M. V.

196671 pp.
Boundary layer measurements in the UTIA 5 - by 7 - inch supersonic wind tunnelJ. Ruptash
⏱ 23m

Boundary layer measurements in the UTIA 5 - by 7 - inch supersonic wind tunnel

J. Ruptash

195223 pp.
On the coupling between a supersonic boundary layer and a flexible surfaceAbdelkader Frendi

On the coupling between a supersonic boundary layer and a flexible surface

Abdelkader Frendi

1992No page data
Porous and microporous honeycomb composites as potential boundary-layer bleed materialsD. O. Davis

Porous and microporous honeycomb composites as potential boundary-layer bleed materials

D. O. Davis

1997No page data
Numerical calculations of shock-wave/boundary-layer flow interactionsP. G. Huang

Numerical calculations of shock-wave/boundary-layer flow interactions

P. G. Huang

1994No page data
Non-linear evolution of a second mode wave in supersonic boundary layersGordon Erlebacher

Non-linear evolution of a second mode wave in supersonic boundary layers

Gordon Erlebacher

1989No page data
Nonparallel instability of supersonic and hypersonic boundary layersNabil M. El-Hady
⏱ 55m

Nonparallel instability of supersonic and hypersonic boundary layers

Nabil M. El-Hady

199155 pp.
Görtler vortices and transition in wall boundary layers of two Mach 5 nozzlesIvan E. Beckwith
⏱ 1h 9m

Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles

Ivan E. Beckwith

198169 pp.
Effects of probe size on measurements in a laminar boundary layer in supersonic flowG. R. Ludwig

Effects of probe size on measurements in a laminar boundary layer in supersonic flow

G. R. Ludwig

1956No page data
Fixing boundary-layer transition on supersonic-wind-tunnel models (II)Marvin Luther
⏱ 1h 34m

Fixing boundary-layer transition on supersonic-wind-tunnel models (II)

Marvin Luther

195694 pp.
Surface documentation of a 3-D supersonic, shock-wave-boundary layer interactionUnknown Author

Surface documentation of a 3-D supersonic, shock-wave-boundary layer interaction

Unknown Author

1994No page data
Laser Doppler vellcimeter measurements of boundary layer velocity and turbulent intensities in MACH 2.5 flowJesse Sewell

Laser Doppler vellcimeter measurements of boundary layer velocity and turbulent intensities in MACH 2.5 flow

Jesse Sewell

1994No page data
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