Subsonic and supersonic hinge-moment and effectiveness characteristics of an unbalanced lateral control having low theoretical hinge moments at supersonic speeds
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Goin, Kennith L↗
Engineering topics
Goin, Kennith L
Publications and source records attributed to Goin, Kennith L.
Effects of Trailing-edge Bluntness on the Lift, Drag, and Pitching-moment Characteristics of Unswept, 45 Degree Swept, and 45 Degree Delta Wings at Mach Numbers of 1.41, 1.62, and 1.96
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Goin, Kennith L↗
Theoretical analyses to determine unbalanced trailing-edge controls having minimum hinge moments due to deflection at supersonic speeds
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Goin, Kennith L↗
Effects of Plan Form, Airfoil Section, and Angle of Attack on the Pressures Along the Base of Blunt-trailing-edge Wings at Mach Numbers of 1.41, 1.62, and 1.96
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Goin, Kennith L↗
Equations and charts for the rapid estimation of hinge-moment and effectiveness parameters for trailing-edge controls having leading and trailing edges swept ahead of the Mach lines
Existing conical-flow solutions have been used to calculate the hinge-moments and effectiveness parameters of trailing-edge controls having leading and trailing edges swept ahead of the Mach lines and having streamwise root and tip chords. Equations and detailed charts are presented for the rapid estimation of these parameters. Also included is an approximate method by which these parameters may be corrected for airfoil-section thickness.
Goin, Kennith L↗
Investigation at a Mach number of 1.9 and a Reynolds number of 2.2 x 10(exp 6) of several flap-type lateral-control devices on a wing having 42.7 degrees sweepback of the leading edge
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Goin, Kennith L↗
Experimental and calculated hinge moments of two ailerons on a 42.7 degrees sweptback wing at a Mach number of 1.9
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Goin, Kennith L↗