An Investigation of Sting Interference Effects on an Oscillating Cone in Transonic Flow

Wind tunnel sting support interference effects on dynamic stability derivatives, static pitching moment and base pressure of a blunt, 7-deg cone were investigated at subsonic and transonic Mach numbers. The cone was tested with sting configurations having a variable effective sting length ranging fr...

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Bibliographische Detailangaben
1. Verfasser:	Cyran, Frederic B
Format:	Report
Sprache:	eng
Schlagworte:	AERODYNAMIC STABILITY ANGLE OF ATTACK BASE PRESSURE CONICAL BODIES CRITICAL LENGTH DAMPING DATA REDUCTION DYNAMIC STABILITY TESTS EXPERIMENTAL DATA EXPERIMENTAL DESIGN FLOW FIELDS Fluid Mechanics INTERFERENCE LENGTH LPN- AAO-P41C-A9 LPN-ARO-V32F-09 MOMENTS OSCILLATION PE65807F PITCH(MOTION) REYNOLDS NUMBER SLENDER BODIES STING MOUNTS SUPPORTS Test Facilities, Equipment and Methods THESES TRANSONIC FLOW TURBULENT BOUNDARY LAYER WIND TUNNEL MODELS
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