Books on the topic 'High angle of attack'

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.

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.

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.

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.

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.

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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

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. National Aeronautics and Space Administration, Langley Research Center, 1990.

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.

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.

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.

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.

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.

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.

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.

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, 1995.

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, 1995.

Hugh L. Dryden Flight Research Center., ed. High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test. National Aeronautics and Space Administration, Dryden Flight Research Center, 1994.

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.

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

Center, Langley Research, ed. High angle of attack position sensing for the Southampton University Magnetic Suspension and Balance System. National Aeronautics and Space Administration, Langley Research Center, 1987.

Hugh L. Dryden Flight Research Center., ed. High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test. National Aeronautics and Space Administration, Dryden Flight Research Center, 1994.

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.

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.

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, 1995.

N, Clark Robert, Burken John J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Flight test of the X-29A at high angle of attack: Flight dynamics and controls. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.