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stability of airplanes longitudinal

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View Longitudinal-control design approach for high-angle-of-attack aircraft By Aaron J. Ostroff

Longitudinal-control design approach for high-angle-of-attack aircraft

Longitudinal-control design approach for high-angle-of-attack aircraft

By Aaron J. Ostroff

View Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration By Paul L. Coe

Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration

Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration

By Paul L. Coe

View Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration By Lawrence E. Putnam

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration

Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration

By Lawrence E. Putnam

View Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth By David L. I. Kirkpatrick

Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth

Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth

By David L. I. Kirkpatrick

View Flight measurements to determine effect of a spring-loaded tab on longitudinal stability of an airplane By Langley Aeronautical Laboratory

Flight measurements to determine effect of a spring-loaded tab on longitudinal stability of an airplane

Flight measurements to determine effect of a spring-loaded tab on longitudinal stability of an airplane

By Langley Aeronautical Laboratory

View Effects of static margin and rotational damping in pitch on the longitudinal stability characteristics of an airplane as determined by tests of a model in the NACA free-flight tunnel By Langley Aeronautical Laboratory

Effects of static margin and rotational damping in pitch on the longitudinal stability characteristics of an airplane as determined by tests of a model in the NACA free-flight tunnel

Effects of static margin and rotational damping in pitch on the longitudinal stability characteristics of an airplane as determined by tests of a model in the NACA free-flight tunnel

By Langley Aeronautical Laboratory

View Redesign of a variable-gain output feedback longitudinal controller flown on the High-Alpha Research Vehicle (HARV) By Aaron J. Ostroff

Redesign of a variable-gain output feedback longitudinal controller flown on the High-Alpha Research Vehicle (HARV)

Redesign of a variable-gain output feedback longitudinal controller flown on the High-Alpha Research Vehicle (HARV)

By Aaron J. Ostroff

View Theroetical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack By James M Luckring

Theroetical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack

Theroetical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack

By James M Luckring

View Simulator study of stall/post-stall characteristics of a fighter airplane with longitudinal static stability By

Simulator study of stall/post-stall characteristics of a fighter airplane with longitudinal static stability

Simulator study of stall/post-stall characteristics of a fighter airplane with longitudinal static stability

By

View Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data By William T. Suit

Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data

Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data

By William T. Suit

View Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA) By Jack D. Stephenson

Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA)

Longitudinal stability and control characteristics of the Quiet Short-Haul Research Aircraft (QSRA)

By Jack D. Stephenson

View The interference of the model support mast with measurements of the longitudinal and lateral aerodynamic coefficients By C. Van de Kreeke

The interference of the model support mast with measurements of the longitudinal and lateral aerodynamic coefficients

The interference of the model support mast with measurements of the longitudinal and lateral aerodynamic coefficients

By C. Van de Kreeke

View Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data By William T. Suit

Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data

Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data

By William T. Suit

View Analysis of oscillatory motion of a light airplane at high values of lift coefficient By James G Batterson

Analysis of oscillatory motion of a light airplane at high values of lift coefficient

Analysis of oscillatory motion of a light airplane at high values of lift coefficient

By James G Batterson

View An introduction to the longitudinal static stability of low-speed aircraft By F. G. Irving

An introduction to the longitudinal static stability of low-speed aircraft

An introduction to the longitudinal static stability of low-speed aircraft

By F. G. Irving