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Laminar boundary layer
Laminar flow 42
Boundary layer 31
Turbulent boundary layer 29
Boundary layer control 25
Heat 25
Transmission 24
Mathematics 20
Air flow 16
Boundary layer transition 16
Mathematical analysis 16
Plates (Engineering) 16
Aerodynamics, Supersonic 15
Aerodynamics 14
Aerofoils 11
Boundary layer stability 11
Mathematical models 10
Shock waves 10
Turbulence 10
Cooling 8
Equations 8
Aerodynamic heating 7
Boundary layer flow 7
Skin friction (Aerodynamics) 7
Wind tunnel tests 7
Wings 7
Aerodynamic load 6
Airplanes 6
Angle of attack (Aerodynamics) 6
Cone 6

Experimental and theoretical studies of area suction for the control of the laminar boundary layer on a porous bronze NACA 64A010 airfoil / by Burrows, Dale L.

Investigation of laminar boundary layer in compressible fluids using the Crocco method / by Van Driest, E. R.

Laminar friction and heat transfer at Mach numbers from 1 to 10 / by Klunker, E. B.

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

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

On the stability of the free laminar boundary layer between parallel streams / by Lessen, Martin

The interactions of a flame and its self-induced boundary layer by Ott, James D.

Unsteady laminar boundary-layer flow / by Moore, F. K. (Franklin K.)

Laminar boundary layer on a circular cone in supersonic flow at a small angle of attack / by Moore, F. K. (Franklin K.)

Simplified method for calculation of compressible laminar boundary layer with arbitrary free-stream pressure gradient / by Low, George M., 1926-1984

Three-dimensional compressible laminar boundary-layer flow / by Moore, F. K. (Franklin K.)

An approximate method for determining the displacement effects and viscous drag of laminar boundary layers in two-dimensional hypersonic flow / by Bertram, Mitchel H.

Study of the pressure rise across shock waves required to separate laminar and turbulent boundary layers / by Donaldson, Coleman duP

A flight investigation of the effect of shape and thickness of the boundary layer on the pressure distribution in the presence of shock / by Harrin, Eziaslav N.

Experimental investigation at a Mach number of 2.41 of average skin-friction coefficients and velocity profiles for laminar and turbulent boundary layers and an assessment of probe... by O'Donnell, Robert M.

Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperature / by Donoughe, Patrick L.

Method for calculation of compressible laminar boundary layer with axial pressure gradient and heat transfer / by Libby, Paul A.

Present status of information relative to the prediction of shock-induced boundary-layer separation / by Lange, Roy H.

A flight investigation of laminar and turbulent boundary layers passing through shock waves at full-scale Reynolds numbers / by Harrin, Eziaslav N.

Cooling requirements for stability of laminar boundary layer with small pressure gradient at supersonic speeds / by Low, George M., 1926-1984

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Experimental and theoretical studies of area suction for the control of the laminar boundary layer on a porous bronze NACA 64A010 airfoil / by Burrows, Dale L.

Investigation of laminar boundary layer in compressible fluids using the Crocco method / by Van Driest, E. R.

Laminar friction and heat transfer at Mach numbers from 1 to 10 / by Klunker, E. B.

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

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

On the stability of the free laminar boundary layer between parallel streams / by Lessen, Martin

The interactions of a flame and its self-induced boundary layer by Ott, James D.

Unsteady laminar boundary-layer flow / by Moore, F. K. (Franklin K.)

Laminar boundary layer on a circular cone in supersonic flow at a small angle of attack / by Moore, F. K. (Franklin K.)

Simplified method for calculation of compressible laminar boundary layer with arbitrary free-stream pressure gradient / by Low, George M., 1926-1984

Three-dimensional compressible laminar boundary-layer flow / by Moore, F. K. (Franklin K.)

An approximate method for determining the displacement effects and viscous drag of laminar boundary layers in two-dimensional hypersonic flow / by Bertram, Mitchel H.

Study of the pressure rise across shock waves required to separate laminar and turbulent boundary layers / by Donaldson, Coleman duP

A flight investigation of the effect of shape and thickness of the boundary layer on the pressure distribution in the presence of shock / by Harrin, Eziaslav N.

Experimental investigation at a Mach number of 2.41 of average skin-friction coefficients and velocity profiles for laminar and turbulent boundary layers and an assessment of probe... by O'Donnell, Robert M.

Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperature / by Donoughe, Patrick L.

Method for calculation of compressible laminar boundary layer with axial pressure gradient and heat transfer / by Libby, Paul A.

Present status of information relative to the prediction of shock-induced boundary-layer separation / by Lange, Roy H.

A flight investigation of laminar and turbulent boundary layers passing through shock waves at full-scale Reynolds numbers / by Harrin, Eziaslav N.

Cooling requirements for stability of laminar boundary layer with small pressure gradient at supersonic speeds / by Low, George M., 1926-1984

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