Books on the topic 'High angle of attack'

Rom, Josef. High Angle of Attack Aerodynamics. New York, NY: Springer New York, 1992. http://dx.doi.org/10.1007/978-1-4612-2824-0.

Kawamura, R., and Y. Aihara, eds. Fluid Dynamics of High Angle of Attack. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-642-52460-8.

High angle of attack aerodynamics: Subsonic, transonic, and supersonic flows. New York: Springer-Verlag, 1991.

Ostroff, Aaron J. Longitudinal-control design approach for high-angle-of-attack aircraft. Hampton, Va: Langley Research Center, 1993.

High Angle of Attack Aerodynamics: Subsonic, Transonic, and Supersonic Flows. New York, NY: Springer New York, 1992.

Ostroff, Aaron J. Longitudinal-control design approach for high-angle-of-attack aircraft. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Katz, Joseph. Impulsive start of a symmetric airfoil at high angle of attack. [Washington, DC: National Aeronautics and Space Administration, 1996.

Hwang, Danny P. A numerical analysis applied to high angle of attack three-dimensional inlets. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Johnson, Dan A. Flowfield measurements in the wake of a missile at high angle of attack. Monterey, Calif: Naval Postgraduate School, 1989.

Whitmore, Stephen A. Development of a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1991.

Klein, Vladislav. Aerodynamic parameters of high-angle-of-attack research vehicle (Harv) estimated from flight data. Hampton, Va: National Aeronautics and Space Administration, 1990.

Klein, Vladislav. Aerodynamic parameters of High-Angle-of-Attack Research Vehicle (HARV) estimated from flight data. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Matsuo, N. Aerodynamic characteristics of general aviation at high angle of attack with the propeller slipstream. Washington DC: National Aeronautics and Space Administration, 1987.

Bauer, Jeffrey E. Flight test of the X-29A at high angle of attack: flight dynamics and controls. Edwards, Calif: Dryden Flight Research Facility, 1995.

Wallace, Lane E. Nose up: High angle-of-attack and thrust vectoring research at NASA Dryden, 1979-2001. Washington, D.C: National Aeronautics and Space Administration, NASA History Office, 2004.

Lung, Ming-Hung. Flowfield measurements in the vortex wake of a missile at high angle of attack in turbulence. Monterey, Calif: Naval Postgraduate School, 1988.

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Moon, Young J. Numerical simulation by TVD schemes of complex shock reflections from airfoils at high angle of attack. New York: American Institute of Aeronautics and Astronautics, 1987.

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center, 1996.

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. Washington, D.C: National Aeronautics and Space Administration, 1996.

Jorden, Frank L. Wind-tunnel static and free-flight investigation of high-angle-of attack stability and control characteristics of a model of the EA-6B airplane. Hampton, Va: Langley Research Center, 1992.

Freudinger, Lawrence C. Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Steenken, William G. An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft. Edwards, Calif: NASA Dryden Flight Research Center, 1997.

Mathre, John Mark. Computational investigation of incompressible airfoil flows at high angles of attack. Monterey, Calif: Naval Postgraduate School, 1988.

Ostroff, Aaron J. Application of variable-gain output feedback for high-alpha control. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Ostroff, Aaron J. Application of variable-gain output feedback for high-alpha control. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Center, Langley Research, ed. A High angle of attack inviscid shuttle orbiter computation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Rom, Josef. High Angle of Attack Aerodynamics: Subsonic, Transonic, and Supersonic Flows. Springer, 1992.

S, Proffitt Melissa, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Longitudinal-control design approach for high-angle-of-attack aircraft. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

High Angle of Attack Aerodynamics: Subsonic, Transonic, and Supersonic Flows. Springer, 2012.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Actuator and aerodynamic modeling for high-angle-of-attack aeroservoelasticity. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration., ed. High angle-of-attack aerodynamic characteristics of crescent and elliptic wings. Davis, CA: University of California, Dept. of Mechanical Engineering, Division of Aeronautical Science and Engineering, 1989.

United States. National Aeronautics and Space Administration., ed. High angle-of-attack aerodynamic characteristics of crescent and elliptic wings. Davis, CA: University of California, Dept. of Mechanical Engineering, Division of Aeronautical Science and Engineering, 1989.

Victoria, Regenie, and Dryden Flight Research Facility, eds. The F-18 High Alpha Research Vehicle: A high-angle-of-attack testbed aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

Victoria, Regenie, and Dryden Flight Research Facility, eds. The F-18 High Alpha Research Vehicle: A high-angle-of-attack testbed aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

Ultra high bypass nacelle areodynamics: Inlet flow-through high angle of attack distortion test. [Washington, DC: National Aeronautics and Space Administration, 1992.

A, Regenie Victoria, and Dryden Flight Research Facility, eds. The F-18 High Alpha Research Vehicle: A high-angle-of-attack testbed aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

A, Regenie Victoria, and Dryden Flight Research Facility, eds. The F-18 High Alpha Research Vehicle: A high-angle-of-attack testbed aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

N, Pedreiro, Joint Institute for Aeronautics and Acoustics., and United States. National Aeronautics and Space Administration., eds. Roll-yaw control at high angle of attack by forebody tangential blowing. [Stanford, Calif.?]: Joint Institute for Aeronautics and Acoustics, 1995.

N, Pedreiro, Joint Institute for Aeronautics and Acoustics., and United States. National Aeronautics and Space Administration., eds. Roll-yaw control at high angle of attack by forebody tangential blowing. [Stanford, Calif.?]: Joint Institute for Aeronautics and Acoustics, 1995.

N, Pedreiro, Joint Institute for Aeronautics and Acoustics., and United States. National Aeronautics and Space Administration., eds. Roll-yaw control at high angle of attack by forebody tangential blowing. [Stanford, Calif.?]: Joint Institute for Aeronautics and Acoustics, 1995.

N, Pedreiro, Joint Institute for Aeronautics and Acoustics., and United States. National Aeronautics and Space Administration., eds. Roll-yaw control at high angle of attack by forebody tangential blowing. [Stanford, Calif.?]: Joint Institute for Aeronautics and Acoustics, 1995.

An Improved Method for Predicting Axial Force at High Angle of Attack. Storming Media, 1997.

V, Foster John, and Langley Research Center, eds. Development of a preliminary high-angle-of-attack nose-down pitch control requirement for high-performance aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

D, Wichman Keith, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. High-alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

W, Banks Daniel, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. The F/A-18 high-angle-of-attack ground-to-flight correlation: Lessons learned. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

A, Gazzaniga John, and United States. National Aeronautics and Space Administration., eds. Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack. [Washington, DC]: National Aeronautics and Space Administration, 1989.

The F/A-18 high-angle-of-attack ground-to-flight correlation: Lessons learned. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.