Unsteady Aerodynamics - Work Unit 2300-FF-07

This task addressed basic research to better understand unsteady, separated flows and to utilize this understanding to develop innovative concepts to control unsteady aerodynamic phenomena to enhance flight vehicle maneuverability. This effort sought to expand the flight performance boundaries by de...

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Bibliographische Detailangaben
1. Verfasser:	Stephen, Eric J
Format:	Report
Sprache:	eng
Schlagworte:	AERODYNAMIC FORCES AERODYNAMIC STABILITY Aerodynamics ANGLE OF ATTACK BOUNDARY LAYER COMPARISON COMPUTATIONAL FLUID DYNAMICS COMPUTERIZED SIMULATION DELTA WINGS EXPERIMENTAL DATA FIGHTER AIRCRAFT FLIGHT ENVELOPE FLIGHT MANEUVERS FLOW FIELDS FLOW SEPARATION FLOW VISUALIZATION Fluid Mechanics FOREBODIES GAS SURFACE INTERACTIONS NAVIER STOKES EQUATIONS NEURAL NETS PITCH(MOTION) PRESSURE DISTRIBUTION STALLING TAILS(AIRCRAFT) THREE DIMENSIONAL FLOW TWO DIMENSIONAL FLOW UNSTEADY FLOW VORTICES WAKE WING BODY CONFIGURATIONS WUAFMC2300FF07
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