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Low-speed wind-tunnel measurements of the oscillatory lateral stability derivatives for a model of a slender aircraft (HP 115) including the effects of frequency parameter
J. S. Thompson
;
R. A. Fail
;
J. V. Inglesby
(
1969
)
Measurements of oscillatory derivatives at mach numbers up to 2.6 on a model of a supersonic transport design study (Bristol type 198)
J. S. Thompson
;
R. A. Fail
(
1965
)
Oscillatory-derivative measurements on sting-mounted wind-tunnel models method of test and results for pitch and yaw on a cambered ogee wing at mach numbers up to 2.6
J. S. Thompson
;
R. A. Fail
(
1962
)
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J. S. Thompson (3)
R. A. Fail (3)
J. V. Inglesby (1)
Date Issued
1969 (1)
1965 (1)
1962 (1)