Books on the topic 'Attack angle'

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

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

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. 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. University of California, Dept. of Mechanical Engineering, Division of Aeronautical Science and Engineering, 1989.

United States. National Aeronautics and Space Administration., ed. Prediction of the noise from a propeller at angle of attack. National Aeronautics and Space Administration, 1990.

United States. National Aeronautics and Space Administration., ed. Prediction of noise field of a propfan at angle of attack. National Aeronautics and Space Administration, 1991.

Center, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. The radiation of sound from a propeller at angle of attack. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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

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

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

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. 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. 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. 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. Joint Institute for Aeronautics and Acoustics, 1995.

United States. National Aeronautics and Space Administration., ed. Cruise noise of counterrotation propeller at angle of attack in wind tunnel. National Aeronautics and Space Administration, 1987.

M, Nallasamy, and United States. National Aeronautics and Space Administration., eds. Near-field noise of a single-rotation propfan at an angle of attack. National Aeronautics and Space Administration, 1990.

M, Nallasamy, and United States. National Aeronautics and Space Administration., eds. Near-field noise of a single-rotation propfan at an angle of attack. National Aeronautics and Space Administration, 1990.

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

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

1918-, Kawamura R., Aihara Y. 1933-, International Union of Theoretical and Applied Mechanics., and IUTAM Symposium on Fluid Dynamics of High Angle of Attack (1992 : Tokyo, Japan), eds. Fluid dynamics of high angle of attack: IUTAM symposium Tokyo, Japan, September 13-17, 1992. Springer-Verlag, 1993.

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. Langley Research Center, 1992.

A, Whitmore Stephen, Dryden Flight Research Facility, and AIAA Aerospace Sciences Meeting (29th : 1991 : Reno, Nevada), eds. Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flights. National Aeronautics and Space Administration, Ames Resarch Center, Dryden Flight Research Facility, 1991.

W, Banks Daniel, and Hugh L. Dryden Flight Research Center., eds. The F/A-18 high-angle-of-attack ground-to-flight correlation: Lessons learned. 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. National Aeronautics and Space Administration, 1989.

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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

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

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

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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

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

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. National Aeronautics and Space Administration, 1989.

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. National Aeronautics and Space Administration, 1989.

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

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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

A, Whitmore Stephen, and Dryden Flight Research Facility, eds. High-angle-of-attack pneumatic lag and upwash corrections for a hemispherical flow direction sensor. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1987.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of the flow about the F-18 HARV at high angle of attack. MCAT Institute, 1994.

F, Groeneweg J., and Lewis Research Center, eds. Prediction of unsteady blade surface pressures on an advanced propeller at an angle of attack. Lewis Research Center, 1989.

A, Whitmore Stephen, and Dryden Flight Research Facility, eds. High-angle-of-attack pneumatic lag and upwash corrections for a hemispherical flow direction sensor. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1987.

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

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