1-22 of 22 Books
X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
By Kenneth W. Iliff
Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
By Kenneth W. Iliff
Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
By Kenneth W. Iliff
Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes
Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes
By Robert J. Foley
Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft
Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft
By Scott P. Fears
Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
By A. B. Blair
Performance at transonic speeds of an attitude sensing head using short protruding tubes
Performance at transonic speeds of an attitude sensing head using short protruding tubes
By D. A. Secomb
Performance of an 0.81 in. diameter hemisphere-cylinder yawmeter at transonic speeds and varying Reynolds number
Performance of an 0.81 in. diameter hemisphere-cylinder yawmeter at transonic speeds and varying Reynolds number
By D. A. Secomb
Measurements at transonic speeds of the sideforce & yawing moment on various store arrangements mounted beneath a 45⁰ swept wing-fuselage model
Measurements at transonic speeds of the sideforce & yawing moment on various store arrangements mounted beneath a 45⁰ swept wing-fuselage model
By Philip Marsden
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
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
By Kenneth W. Iliff
Measurement of the yawing moment and product of inertia of an aircraft by the single point suspension method
Measurement of the yawing moment and product of inertia of an aircraft by the single point suspension method
By Alan Anthony Woodfield
Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model
Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model
By A. P. Cox
Emergency flight control using only engine thrust and lateral center-of-gravity offset
Emergency flight control using only engine thrust and lateral center-of-gravity offset
By
Analysis of rotary balance data for the F-15 airplane including the effect of conformal fuel tanks
Analysis of rotary balance data for the F-15 airplane including the effect of conformal fuel tanks
By Billy Barnhart
Linearized model for wind turbines in yaw
Linearized model for wind turbines in yaw
By Somsak Chaiyapinunt
Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
By A. B Blair
A new satellite instrument for yaw and pitch measurements
A new satellite instrument for yaw and pitch measurements
By J. P McIsaac
Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
By Mary L. Mason
Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes
Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes
By Mary L. Mason
Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
By Elizabeth B. Plentovich
Evaluation of circulation control tail boom for yaw control
Evaluation of circulation control tail boom for yaw control
By A. H. Logan
Results of a feasibility study for determining the yaw angle of a landing aircraft
Results of a feasibility study for determining the yaw angle of a landing aircraft
By F. Donald Queen