AIAA Atmospheric Flight Mechanics Conference, Hilton Head Island, SC, Aug. 10-12, 1992, Technical Papers. Pts. 1-2

Conference · Wed Jan 01 00:00:00 EST 1992

OSTI ID:7162846

Consideration is given to aircraft dynamics and aerodynamics in atmospheric disturbances, vehicle trajectory optimization, projectile and missile flight dynamics, high alpha prediction codes for flow phenomenon, aircraft handling qualities, high alpha CFD and control, aircraft agility, unsteady flow phenomenon, parameter estimation, hypersonic technology, CFD for store separation, aeroassist technology, and unsteady and high alpha numerical studies. Particular attention is given to optimal recovery from microburst wind shear, optimal trajectories for an unmanned air-vehicle in the horizontal plane, numerical simulation of missile flow fields, pulsating spanwise blowing on a fighter aircraft, pilot control identification using minimum model error estimation, Navier-Stokes computations for oscillating control surfaces, aircraft agility maneuvers, fin motion after projectile exit from gun tube, the vortical structure in the wake during dynamic stall, nonlinear aerodynamic parameter estimation, missile and spacecraft coning instabilities, 3D Euler solutions on wing-pylon-store configuration with unstructured tetrahedral meshes, and a simulation model for tail rotor failure.

• OSTI ID: 7162846
• Report Number(s): CONF-920845-
• Resource Relation: Conference: American Institute of Aeronautics and Astronautics (AIAA) meeting, Hilton Head, SC (United States), 10-12 Aug 1992
• Country of Publication: United States
• Language: English

Related Subjects

45 MILITARY TECHNOLOGY, WEAPONRY, AND NATIONAL DEFENSE
AIRCRAFT
AERODYNAMICS
MISSILES
COMPUTERIZED SIMULATION
CONTROL
FINITE ELEMENT METHOD
FLIGHT TESTING
LEADING ABSTRACT
MEETINGS
OPTIMIZATION
STABILITY
TRAJECTORIES
WIND
ABSTRACTS
CALCULATION METHODS
DOCUMENT TYPES
FLUID MECHANICS
MECHANICS
NUMERICAL SOLUTION
SIMULATION
TESTING
450000* - Military Technology
Weaponry
& National Defense