AIAA Applied Aerodynamics Conference, 6th, Williamsburg, VA, June 6-8, 1988, Technical Papers

Conference · Thu Dec 31 23:00:00 EST 1987

OSTI ID:6839507

The present conference on applied aerodynamics discusses the flowfield for the propeller disks of a twin-pusher canard configuration, the effects of canard-wing flowfield interactions on longitudinal stability and potential deep-stall trim, the progress of wing vortex flows to vortex breakdown, flow visualization by IR imaging, wind tunnel investigation of wing-in-ground effects, three-dimensional windmill surface pressure calculations, the base drag of highly maneuvering nonthrusting missiles, riblet drag reduction at flight conditions, and calculations of hypersonic transitional flow over cones. Also discussed are the roll characteristics of finned projectiles, the design of low Reynolds number airfoils, a comparative study of vortex structures, three-dimensional hypersonic nonequilibrium flows at large angles-of-attack, the analysis of wing rock due to forebody vortices, and the influence of small surface discontinuities in turbulent boundary layers.

• OSTI ID: 6839507
• Report Number(s): CONF-8806202-
• Country of Publication: United States
• Language: English

Related Subjects

640410* -- Fluid Physics-- General Fluid Dynamics
75 CONDENSED MATTER PHYSICS
SUPERCONDUCTIVITY AND SUPERFLUIDITY
ABSTRACTS
AERODYNAMICS
AIR TRANSPORT
AIRFOILS
COORDINATES
DOCUMENT TYPES
DRAG
FLUID FLOW
FLUID MECHANICS
HYPERSONIC FLOW
LEADING ABSTRACT
MACHINERY
MECHANICS
MEETINGS
SUPERSONIC TRANSPORT
TRANSPORT
TUNNELS
TURBINES
TURBOMACHINERY
UNDERGROUND FACILITIES
UNSTEADY FLOW
USES
VORTICES
WIND TUNNELS
WIND TURBINES