AIAA Applied Aerodynamics Conference, 8th, Portland, OR, Aug. 20-22, 1990, Technical Papers. Parts 1 2
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-; TRN: 90-036239
- Resource Relation:
- Conference: 1990 AIAA guidance, navigation and control conference, Portland, OR (USA), 20-22 Aug 1990
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
SUPERCONDUCTIVITY AND SUPERFLUIDITY
42 ENGINEERING
AERODYNAMICS
MEETINGS
AIRCRAFT
AIRFOILS
BOUNDARY LAYERS
CALCULATION METHODS
COORDINATES
FLIGHT TESTING
FLUID MECHANICS
INTERACTIONS
LAMINAR FLOW
MESH GENERATION
MISSILES
ROTORS
SHOCK WAVES
SUPERSONIC FLOW
TRANSITION FLOW
VORTICES
WIND TUNNELS
FLUID FLOW
LAYERS
MECHANICS
TESTING
TUNNELS
UNDERGROUND FACILITIES
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