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Supersonic aerodynamic characteristics of a tail-control cruciform maneuverable missile with and without wingsThe aerodynamic characteristics for a winged and a wingless cruciform missile are examined. The body was an ogive-cylinder with a 3.5 caliber forebody; an overall length-to-diameter ratio of 11.667; and has cruciform tails that were trapexoidal in planform. Tests were made both with and without 72.9 deg cruciform delta wings. The investigation was made for Mach numbers from 1.50 to 4.63, roll attitudes of 0 and 45 deg, angles of attack from -40 to 22 deg, and tail control deflections from 10 to -40 deg. The purpose is to determine the influence of the aerodynamic behavior on the design choice for maneuverable missiles intended primarily for air-to-air or surface-to-surface missions. The results indicate that the winged missile with its more linear aerodynamic characteristics and higher lift-curve slope, should provide the highest maneuverability over a large operational range.
Document ID
19780062635
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Spearman, M. L.
(NASA Langley Research Center Hampton, VA, United States)
Fournier, R. H.
(NASA Langley Research Center High-Speed Aerodynamics Div., Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 78-1351
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference
Location: Palo Alto, CA
Start Date: August 7, 1978
End Date: August 9, 1978
Accession Number
78A46544
Distribution Limits
Public
Copyright
Other

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