Explore Books on
spin (aerodynamics)
1-24 of 47 Books
Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft
Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft
By E. Richard White
Spin-tunnel investigation of a 1/13-scale model of the NASA AD-1 oblique-wing research aircraft
Spin-tunnel investigation of a 1/13-scale model of the NASA AD-1 oblique-wing research aircraft
By William L White
A spin-recovery parachute system for light general-aviation airplanes
A spin-recovery parachute system for light general-aviation airplanes
By Charles F. Bradshaw
Spin-tunnel investigation of the spinning characteristics of typical single-engine general aviation airplane designs
Spin-tunnel investigation of the spinning characteristics of typical single-engine general aviation airplane designs
By Sanger M. Burk
Pseudosteady-state analysis of nonlinear aircraft maneuvers
Pseudosteady-state analysis of nonlinear aircraft maneuvers
By John W. Young
Rotary balance data for a single-engine trainer design for an angle-of-attack range of 8 ̊to 90/̊
Rotary balance data for a single-engine trainer design for an angle-of-attack range of 8 ̊to 90/̊
By Paul Pantason
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê
By William Mulcay
Spin-tunnel investigation of a 1/25-scale model of the General Dynamics F-16XL airplane
Spin-tunnel investigation of a 1/25-scale model of the General Dynamics F-16XL airplane
By Raymond D. Whipple
Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊
Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊
By William Bihrle
F-15 rotary balance data for an angle-of-attack range of 8 to 90
F-15 rotary balance data for an angle-of-attack range of 8 to 90
By Billy Barnhart
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20⁰
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20⁰
By J. N. Ralston
Rotary balance data for a single-engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 ̊to 90 ̊
Rotary balance data for a single-engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 ̊to 90 ̊
By William Mulcay
Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30 ̊to 90 ̊
Rotary balance data for a typical single-engine low-wing general aviation design for an angle of attack range 30 ̊to 90 ̊
By William Bihrle
Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG]
Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG]
By William Mulcay
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊
By William Mulcay
Semiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane
Semiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane
By Bandu N. Pamadi
F-15 rotary balance data for an angle-of-attack range of 8p0s to 90p0s
F-15 rotary balance data for an angle-of-attack range of 8p0s to 90p0s
By Billy Barnhart
Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8
Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8
By Billy Barnhart
Spin-tunnel investigation of the spinning characteristics of typical single-engine general aviation airplane designs
Spin-tunnel investigation of the spinning characteristics of typical single-engine general aviation airplane designs
By Sanger M Burk
Spin recovery training
Spin recovery training
By United States. Congress. House. Committee on Science and Technology. Subcommittee on Investigations and Oversight.