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

Conference · Fri Jan 01 00:00:00 EST 1988

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-; TRN: 88-031128
• Resource Relation: Conference: 6. AIAA applied aerodynamics conference, Williamsburg, VA, USA, 6 Jun 1988
• Country of Publication: United States
• Language: English

Related Subjects

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