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control surfaces

1-24 of 65 Books

View The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil By Charles D. Harris

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil

By Charles D. Harris

View Optimal pitch thrust-vector angle and benefits for all flight regimes By Glenn B. Gilyard

Optimal pitch thrust-vector angle and benefits for all flight regimes

Optimal pitch thrust-vector angle and benefits for all flight regimes

By Glenn B. Gilyard

View 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

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

View Control-surface hinge-moment calculations for a high-aspect-ratio supercritical wing By Boyd Perry

Control-surface hinge-moment calculations for a high-aspect-ratio supercritical wing

Control-surface hinge-moment calculations for a high-aspect-ratio supercritical wing

By Boyd Perry

View X-38 vehicle 131 flutter assessment By James P. Smith - undifferentiated

X-38 vehicle 131 flutter assessment

X-38 vehicle 131 flutter assessment

By James P. Smith - undifferentiated

View Navier-Stokes computations on full wing-body configuration with oscillating control surfaces By Shigeru Obayashi

Navier-Stokes computations on full wing-body configuration with oscillating control surfaces

Navier-Stokes computations on full wing-body configuration with oscillating control surfaces

By Shigeru Obayashi

View Microfabricated ice-detection sensor By Russell G. DeAnna

Microfabricated ice-detection sensor

Microfabricated ice-detection sensor

By Russell G. DeAnna

View Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft By

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft

By

View Laser scanning system for pressure and temperature paints By John Sullivan

Laser scanning system for pressure and temperature paints

Laser scanning system for pressure and temperature paints

By John Sullivan

View Wind-tunnel investigation of a full-scale canard-configured general aviation airplane By Long P. Yip

Wind-tunnel investigation of a full-scale canard-configured general aviation airplane

Wind-tunnel investigation of a full-scale canard-configured general aviation airplane

By Long P. Yip

View Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 By L. Roane Hunt

Aerothermal environment in chordwise gaps between split elevons at Mach 6.8

Aerothermal environment in chordwise gaps between split elevons at Mach 6.8

By L. Roane Hunt

View 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 derivates By Kenneth W. Lliff

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 derivates

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 derivates

By Kenneth W. Lliff

View Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft By Robert Navarro

Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft

Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft

By Robert Navarro

View Automated optimum design of wing structures By Rao, S. S.

Automated optimum design of wing structures

Automated optimum design of wing structures

By Rao, S. S.

View Proceedings of the Circulation-Control Workshop, 1986 By Circulation-Control Workshop (1986 Ames Research Center)

Proceedings of the Circulation-Control Workshop, 1986

Proceedings of the Circulation-Control Workshop, 1986

By Circulation-Control Workshop (1986 Ames Research Center)

View Methods for estimating stability and control derivatives of conventional subsonic airplanes By Jan Roskam

Methods for estimating stability and control derivatives of conventional subsonic airplanes

Methods for estimating stability and control derivatives of conventional subsonic airplanes

By Jan Roskam

View A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane By Frederick J. Lallman

A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane

A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane

By Frederick J. Lallman

View Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45⁰ By William P. Henderson

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45⁰

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45⁰

By William P. Henderson

View Precision controllability of the FY-17 airplane By Thomas R. Sisk

Precision controllability of the FY-17 airplane

Precision controllability of the FY-17 airplane

By Thomas R. Sisk

View Non-linear unsteady wing theory By J. E. McCune

Non-linear unsteady wing theory

Non-linear unsteady wing theory

By J. E. McCune

View Testing and optimization of electrically conductive spacecraft coatings By R. J. Mell

Testing and optimization of electrically conductive spacecraft coatings

Testing and optimization of electrically conductive spacecraft coatings

By R. J. Mell

View Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings By Ken Craig

Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings

Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings

By Ken Craig

View Thermal control surfaces experiment By Donald R. Wilkes

Thermal control surfaces experiment

Thermal control surfaces experiment

By Donald R. Wilkes

View Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft By Scott P. Fears

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