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Computation of separated and unsteady flows with one- and two-equation turbulence models
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Lee-side flow over delta wings at supersonic speeds
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The structure of separated flow regions occurring near the leading edge of airfoils, including transition
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Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
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NASA/FAA Tailplane Icing Program
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Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
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Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
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Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
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Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
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Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails
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Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data
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Lateral shock of the R Aquarii jet
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The effects of the critical ice accretion on airfoil and wing performance
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High-lift systems on commercial subsonic airliners
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Space shuttle pinhole formation mechanism studies
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Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters
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F-18 High Alpha Research Vehicle surface pressures
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Control of unsteady separated flow associated with the dynamic stall of airfoils
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Boundary layer transition in the leading edge region of a swept cylinder in high speed flow
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Leading-edge receptivity for blunt-nose bodies
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Numerical simulation of the SOFIA flowfield
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A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region
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Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)
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Closed form equations for the preliminary design of a heat-pipe-cooled leading edge
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