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1
Random response of rectangular panels to the pressure field beneath a turbulent boundary layer in subsonic flows /
Published 1972CONNECT
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2
Influence of the external disturbances on natural transition in boundary layers on NACA0012 airfoil /
Published 2006CONNECT
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3
Boundary layer flow over elastic surfaces : compliant surfaces and combined methods for marine vessel drag reduction /
Published 2013CONNECT
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4
Investigation of materials for boundary layer control in a supersonic wind tunnel /
Published 2013CONNECT
Government Document Electronic eBook -
5
Investigation of active flow control to improve aerodynamic performance of oscillating wings /
Published 2014CONNECT
Government Document Electronic eBook -
6
Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction /
Published 1996CONNECT
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7
Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment /
Published 1988CONNECT
Government Document Electronic eBook -
8
Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system /
Published 1990CONNECT
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9
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10
Preliminary investigation on boundary layer control by means of suction and pressure with the U.S.A. 27 airfoil /
Published 1928CONNECT
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11
The aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction /
Published 1953CONNECT
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12
Investigation of a 0.3-scale jet-transport model having a jet-augmented boundary-layer-control flap with direct-lift control capability /
Published 1969CONNECT
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13
Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted v-tail /
Published 1968CONNECT
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14
Low-density, leading-edge bluntness, and ablation effects on wedge-induced laminar-boundary-layer separation at moderate enthalpies in hypersonic flow /
Published 1968CONNECT
Government Document Electronic eBook -
15
Effect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4 /
Published 1968CONNECT
Government Document Electronic eBook -
16
Experiments with an airfoil model on which the boundary layer is controlled without the use of supplementary equipment /
Published 1931CONNECT
Government Document Electronic eBook