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Boundary layer transition
Wind tunnel tests 23
Laminar boundary layer 16
Turbulent boundary layer 15
Boundary layer control 14
Laminar flow 13
Flow visualization 12
Boundary layer stability 11
Reynolds number 11
Boundary layer flow 9
Airfoils 8
Flight tests 8
Flow distribution 8
Leading edges 8
Turbulent flow 8
Flow measurement 7
Transition flow 7
Computational fluid dynamics 6
Swept wings 6
Aerodynamic heating 5
Aerofoils 5
Boundary layers 5
Cross flow 5
Flat plates 5
Supersonic wind tunnels 5
Aerothermodynamics 4
Angle of attack 4
Boundary layer separation 4
Flow meters 4
Free flow 4

High Reynolds number hybrid laminar flow control (HLFC) flight experiment.

Pegasus wing-glove experiment to document hypersonic crossflow transition measurement system and selected flight results /

Towards understanding the mechanism of receptivity and bypass dynamics in laminar boundary layers

Effect of protuberance shape and orientation on Space Shuttle Orbiter boundary-layer transition by King, Rudolph A.

HyBoLT flight experiment by Chen, Fang-Jenq

Experimental study of boundary layer behavior in a simulated low pressure turbine / by Shyne, Rickey J.

Statistical prediction of laminar-turbulent transition by Rubinstein, Robert

Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at sup... by Kim, Hyun D.

Visualization of in-flight flow phenomena using infrared thermography

Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 / by Hollis, Brian R. (Brian Ray)

Mach number effects on turbine blade transition length prediction / by Boyle, Robert J., Simon, F. F. (Frederick F.)

An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages by Wang, Tiecheng

Supersonic quiet-tunnel development for laminar-turbulent transition research final report for NASA Langley grant NAG-1-1607 / by Schneider, Steven P.

Feasibility study of optical boundary layer transition detection method by Azzazy, M.

Hot film wall shear instrumentation for boundary layer transition research by Schneider, Steven P.

A comparison of computer-generated lift and drag polars for a Wortman airfoil to flight and wind tunnel results final report / by Bowers, Albion H.

Pegasus wing-glove experiment to document hypersonic crossflow transition : measurement systems and selected flight results / by Bertelrud, Arild

Supersonic laminar flow control research semiannual report #2 / by Lo, C. F.

A concept for transition mapping on a 10⁰-cone in the National Transonic Facility using flow-pressure variation by Gartenberg, Ehud

In-flight boundary-layer transition on a large flat plate at supersonic speeds / by Banks, D. W.

Search Results

High Reynolds number hybrid laminar flow control (HLFC) flight experiment.

Pegasus wing-glove experiment to document hypersonic crossflow transition measurement system and selected flight results /

Towards understanding the mechanism of receptivity and bypass dynamics in laminar boundary layers

Effect of protuberance shape and orientation on Space Shuttle Orbiter boundary-layer transition by King, Rudolph A.

HyBoLT flight experiment by Chen, Fang-Jenq

Experimental study of boundary layer behavior in a simulated low pressure turbine / by Shyne, Rickey J.

Statistical prediction of laminar-turbulent transition by Rubinstein, Robert

Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at sup... by Kim, Hyun D.

Visualization of in-flight flow phenomena using infrared thermography

Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 / by Hollis, Brian R. (Brian Ray)

Mach number effects on turbine blade transition length prediction / by Boyle, Robert J., Simon, F. F. (Frederick F.)

An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages by Wang, Tiecheng

Supersonic quiet-tunnel development for laminar-turbulent transition research final report for NASA Langley grant NAG-1-1607 / by Schneider, Steven P.

Feasibility study of optical boundary layer transition detection method by Azzazy, M.

Hot film wall shear instrumentation for boundary layer transition research by Schneider, Steven P.

A comparison of computer-generated lift and drag polars for a Wortman airfoil to flight and wind tunnel results final report / by Bowers, Albion H.

Pegasus wing-glove experiment to document hypersonic crossflow transition : measurement systems and selected flight results / by Bertelrud, Arild

Supersonic laminar flow control research semiannual report #2 / by Lo, C. F.

A concept for transition mapping on a 10⁰-cone in the National Transonic Facility using flow-pressure variation by Gartenberg, Ehud

In-flight boundary-layer transition on a large flat plate at supersonic speeds / by Banks, D. W.

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