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Stability and control of hypersonic waveridersThe longitudinal and lateral stability derivatives of caret-wing waveriders flying on-design are calculated using linear piston theory. The experimental work of Kipke is used to validate the lift and pitch stiffness coefficients. Comparison is also made to the analytical work done by Hui. The calculations are extended to off-design conditions with an attached shock wave using tangent wedge theory. The stability derivatives of a Mach 6 waverider are computed and conclusions about its stability are drawn.
Document ID
19930039258
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tarpley, Christopher (NASA Ames Research Center Moffett Field, CA, United States)
Lewis, Mark J. (Maryland Univ. College Park, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 93-0508
Report Number: AIAA PAPER 93-0508
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A23255
Funding Number(s)
CONTRACT_GRANT: NCA2-611
Distribution Limits
Public
Copyright
Other

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