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Effects of external stores on the air combat capability of a delta wing fighterDelta wing point-design fighters with two pylon mounted missiles and aft tail controls (similar to several Soviet designs) have been investigated for a Mach number range from about 0.6 to 2.0. Whereas minimum drag penalties that are expected with the addition of external stores do occur, the effects at higher lifts, corresponding to maneuvering flight, are less severe and often favorable. The drag-due-to-lift factor is less with stores on although the lift curve slope is unaffected. The longitudinal stability level is reduced by the addition of stores while the pitch control effectiveness is unchanged. The directional stability was generally reduced at subsonic speeds and increased at supersonic speeds by the addition of stores but sufficiently high stability levels are obtainable that are compatible with the longitudinal maneuvering limits. Some examples of the potential maneuvering capability in terms of normal acceleration and turn radius are included.
Document ID
19780034893
Document Type
Conference Paper
Authors
Spearman, M. L. (NASA Langley Research Center Hampton, VA, United States)
Sawyer, W. C. (NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
October 1, 1977
Subject Category
AERODYNAMICS
Meeting Information
Aircraft/Stores Compatibility Symposium(Fort Walton Beach, FL)
Distribution Limits
Public
Copyright
Other