Aerodynamic Stability Technology for Maneuverable Missiles. Volume I. Configuration Aerodynamic Characteristics

This study developed empirical methods to predict aerodynamic characteristics of body-tail, body-wing-tail and body-strake-tail missile configurations. Methods cover the Mach number range from 0.6 to 3.0. Methods cover the individual body and tail characteristics at angles of attack from 0 to 180 de...

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Hauptverfasser:	Aiello, Gennaro F, Bateman, Michael C
Format:	Report
Sprache:	eng
Schlagworte:	AERODYNAMIC CHARACTERISTICS AERODYNAMIC CONFIGURATIONS AERODYNAMIC STABILITY Body strake tail configuration Body tail configuration Body wing tail configuration Fluid Mechanics FUSELAGES Guided Missiles MATHEMATICAL PREDICTION PE62201F Pitch plane PITCH(MOTION) STRAKES TAILS(AIRCRAFT) THRUST VECTOR CONTROL SYSTEMS WINGS
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Beschreibung
Zusammenfassung:	This study developed empirical methods to predict aerodynamic characteristics of body-tail, body-wing-tail and body-strake-tail missile configurations. Methods cover the Mach number range from 0.6 to 3.0. Methods cover the individual body and tail characteristics at angles of attack from 0 to 180 degrees. For winged bodies the methods encompass angles of attack up to about 30 degrees. All mutual interference effects are accounted for, allowing accurate prediction of force and moment coefficients. (Author) See also Volume 2, AD-A068 971.