Libri sul tema "Attack angle"

White, Robin A. Angle of attack. New York: Crown Publishers, 1992.

White, Robin A. Angle of attack. New York: Fawcett Gold Medal, 1993.

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., e Y. Aihara, a cura di. 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.

Angle of attack: Harrison Storms and the race to the moon. New York: W.W. Norton, 1992.

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.

Shefchunas, Thomas. Alpha trainer: Angle of attack : unlocking the mystery of flight : understanding stalls & spins. [Emlenton, PA?: s.n.], 1998.

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.

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.

Nallasamy, M. Unsteady Euler analysis of the flow field of a propfan at an angle of attack. Cleveland, Ohio: Lewis Research Center, 1990.

Wong, Douglas T. Evaluation of electrolytic tilt sensors for measuring model angle of attack in wind tunnel tests. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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.

Sehgal, A. K. Investigation of nose bluntness and angle of attack effects on slender bodies in viscous hypertension flows. Norfolk, Va: Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University, 1991.

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.

Gray, Mike. Angle of Attack. Random House Value Publishing, 1995.

Angle of Attack. Random House Value Publishing, 1995.

Cummings, David R. Angle of Attack. PublishAmerica, 2005.

Angle of Attack. Mallach Productions, LLC, 2017.

Burns, Rex. Angle of Attack (Gabe Wager Mysteries, 3). Americana Publishing, 2003.

Center, Langley Research, a cura di. 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, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., a cura di. 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., a cura di. 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., a cura di. 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., a cura di. 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., a cura di. Prediction of noise field of a propfan at angle of attack. [Washington, DC]: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., a cura di. Prediction of the noise from a propeller at angle of attack. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Angle of Attack: Harrison Storms and the Race to the Moon. Penguin (Non-Classics), 1994.

Center, Lewis Research, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., a cura di. The radiation of sound from a propeller at angle of attack. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Angle of Attack: Harrison Storms and the Race to the Moon. Norton & Company, Incorporated, W. W., 2007.

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