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Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings a correlation with experiment / by McMillin, S. Naomi (Susan Naomi)
Published 1990Call Number: Loading…
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Effect of planform and body on supersonic aerodynamics of multibody configurations by McMillin, S. Naomi (Susan Naomi)
Published 1992Call Number: Loading…Click here to view paper online
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Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber / by McMillin, S. Naomi (Susan Naomi)
Published 1996Call Number: Loading…Online Access
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1998 NASA High-Speed Research Program Aerodynamic Performance Workshop proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C., an...
Published 1999Other Authors: “…McMillin, S. Naomi (Susan Naomi)…”
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5
Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65̊ delta wings varying in leading-edge radius and camber
Published 1996Other Authors: “…McMillin, S. Naomi (Susan Naomi)…”
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Related Subjects
Aerodynamics, Supersonic
Airplanes
Delta wings
Flow visualization
Leading edges
Wings, Triangular
Aerodynamic characteristics
Aerodynamic configurations
Aircraft design
Boundary layer transition
Camber
Camber (Aerofoils)
Civil aviation
Computational fluid dynamics
Engine airframe integration
High speed
NASA programs
Optimization
Pressure ratio
Reynolds number
Supersonic transports