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On the interaction between the shock wave attached to a wedge and freestream disturbances
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Effect of surface waviness on transition in three-dimensional boundary-layer flow
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Effect of curvature on the impact damage characteritiscs and residual strength of composite plates
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Summary report of the orbital X-34 wing static aeroelastic study
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Detailed flow-field measurements over a 75⁰ swept delta wing
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Self-similar compressible free vortices
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Artificial boundary conditions for computation of oscillating external flows
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Measurements in transitional boundary layers under high free-stream turbulence and strong acceleration conditions
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Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer
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Towards enhancing and delaying disturbances in free shear flows
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Water tunnel flow visualization study through poststall of 12 novel planform shapes
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On the freestream matching condition for stagnation point turbulent flows
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Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
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Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction
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Hypersonic flows about a 25 ̊sharp cone
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Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
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Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data
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The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge
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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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Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
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Improved two-equation k - [omega] turbulence models for aerodynamic flows
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Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor
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The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity
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A new methodology for free wake analysis using curved vortex elements
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