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Discover Yawing (Aerodynamics)
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Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model
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Analysis of rotary balance data for the F-15 airplane including the effect of conformal fuel tanks
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Results of a feasibility study for determining the yaw angle of a landing aircraft
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Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
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Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
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Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes
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Evaluation of circulation control tail boom for yaw control
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Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes
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Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
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Performance of an 0.81 in. diameter hemisphere-cylinder yawmeter at transonic speeds and varying Reynolds number
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Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
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Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
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X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
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A new satellite instrument for yaw and pitch measurements
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Measurement of the yawing moment and product of inertia of an aircraft by the single point suspension method
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Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
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Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft
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Measurements at transonic speeds of the sideforce & yawing moment on various store arrangements mounted beneath a 45⁰ swept wing-fuselage model
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Performance at transonic speeds of an attitude sensing head using short protruding tubes
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Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives
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Linearized model for wind turbines in yaw
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