AIAA Applied Aerodynamics Conference, 8th, Portland, OR, Aug. 20-22, 1990, Technical Papers. Parts 1 2

Conference · Sun Dec 31 23:00:00 EST 1989

OSTI ID:6280979

The present conference discusses topics in CFD methods and their validation, vortices and vortical flows, STOL/VSTOL aerodynamics, boundary layer transition and separation, wing airfoil aerodynamics, laminar flow, supersonic and hypersonic aerodynamics, CFD for wing airfoil and nacelle applications, wind tunnel testing, flight testing, missile aerodynamics, unsteady flow, configuration aerodynamics, and multiple body/interference flows. Attention is given to the numerical simulation of vortical flows over close-coupled canard-wing configuration, propulsive lift augmentation by side fences, road-vehicle aerodynamics, a shock-capturing method for multidimensional flow, transition-detection studies in a cryogenic environment, a three-dimensional Euler analysis of ducted propfan flowfields, multiple vortex and shock interaction at subsonic and supersonic speeds, and a Navier-Stokes simulation of waverider flowfields. Also discussed are the induced drag of crescent-shaped wings, the preliminary design aerodynamics of missile inlets, finite wing lift prediction at high angles-of-attack, optimal supersonic/hypersonic bodies, and adaptive grid embedding for the two-dimensional Euler equations.

• OSTI ID: 6280979
• Report Number(s): CONF-900861--
• Country of Publication: United States
• Language: English

Related Subjects

42 ENGINEERING
420400 -- Engineering-- Heat Transfer & Fluid Flow
640410* -- Fluid Physics-- General Fluid Dynamics
75 CONDENSED MATTER PHYSICS
SUPERCONDUCTIVITY AND SUPERFLUIDITY
AERODYNAMICS
AIRCRAFT
AIRFOILS
BOUNDARY LAYERS
CALCULATION METHODS
COORDINATES
FLIGHT TESTING
FLUID FLOW
FLUID MECHANICS
INTERACTIONS
LAMINAR FLOW
LAYERS
MECHANICS
MEETINGS
MESH GENERATION
MISSILES
ROTORS
SHOCK WAVES
SUPERSONIC FLOW
TESTING
TRANSITION FLOW
TUNNELS
UNDERGROUND FACILITIES
VORTICES
WIND TUNNELS