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Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeoff by Massey, Steven James
Hampton, Va. : Hanover, Md. :; Hampton, Va. : Hanover, MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information, 2001Call Number: Loading…
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Aerostructural vortical flow interactions with applications to F/A-18 and F-117 tail buffet by Kandil, Osama A.
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996Other Authors: “…Massey, Steven James…”
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Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow by Kandil, Osama A.
[Washington, D.C.] : [National Aeronautics and Space Administration], 1997Other Authors:Call Number: Loading…
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Implementation of advanced two equation turbulence models in the USM3D unstructured flow solver by Wang, Qunzhen
Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 2000Other Authors: “…Massey, Steven James…”
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Related Subjects
Aeroelasticity
Airplanes
Computational fluid dynamics
Navier-Stokes equation
Wings
Aeroacoustics
Aerofoils
Airfoils
Analysis (mathematics)
Angle of attack
Applications programs (Computers)
Buffeting
Buffeting (Aerodynamics)
Computerized simulation
Finite volume method
Flat plates
Flow characteristics
Flux difference splitting
Inviscid flow
Multiblock grids
Navier-Stokes equations
Noise prediction
Plug nozzles
Tail surfaces
Turbulence models
Unstructured grids (Mathematics)
Viscous flow
Vortex breakdown