Books on the topic 'Aerodynamic angle'

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.

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

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.

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

Center, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Center, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Center, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Center, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Bjarke, Lisa J. A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

Bjarke, Lisa J. A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

Isogai, Koji. Numerical simulation of dynamic stall of NACA0012 airfoil oscillating near static stall angle using the Navier-Stokes equations. Tokyo: National Aerospace Laboratory, 1992.

United States. National Aeronautics and Space Administration., ed. System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality: A dissertation ... [Washington, D.C: National Aeronautics and Space Administration, 1997.

Pamadi, Bandu N. A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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. Edwards, Calif: National Aeronautics and Space Administration, Ames Resarch Center, Dryden Flight Research Facility, 1991.

Julio, Chu, Tracy M. B, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

R, Moes Timothy, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Failure detection and fault management techniques for a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Center, Ames Research, and U.S. Army Aviation and Troop Command., eds. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command, 1994.

Piziali, R. A. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. Moffett Field, Ca: Ames Research Center, 1994.

Center, Ames Research, and U.S. Army Aviation and Troop Command., eds. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command, 1994.

Center, Ames Research, and U.S. Army Aviation and Troop Command., eds. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command, 1994.

Center, Ames Research, and U.S. Army Aviation and Troop Command., eds. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command, 1994.

Center, Langley Research, ed. Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.

Center, Langley Research, ed. Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

M, Ware George, MacConochie Ian O, and Langley Research Center, eds. Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

K, Kapania Rakesh, Barthelemy Jean-Francois M, and United States. National Aeronautics and Space Administration., eds. Sensitivity analysis of flutter response of a wing incorporating finite-span corrections. [Washington, DC: National Aeronautics and Space Administration, 1994.

Old Dominion University. Research Foundation. and United States. National Aeronautics and Space Administration., eds. Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application: Final report for the period of December 1, 1996-November 30, 1997 : under research grant NAG-1-648. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University, 1997.

Old Dominion University. Research Foundation. and United States. National Aeronautics and Space Administration., eds. Aeroelastic, CFD, and dynamic computation and optimization for buffet and flutter application: Final report for the period of December 1, 1996-Novemeber 30, 1997 : under research grant NAG-1-648. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering and Technology, Old Dominion University, 1997.

Whipple, Raymond D. Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and sideslip. Hampton, Va: Langley Research Center, 1986.

Hahne, David E. Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Center, Langley Research, ed. Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Center, Langley Research, ed. Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Center, Langley Research, ed. Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

E, McGrath Brian, and Langley Research Center, eds. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Catlin, Gregory M. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Catlin, Gregory M. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

L, Ricket Jonathan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

L, Ricket Jonathan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

L, Ricket Jonathan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

George C. Marshall Space Flight Center., ed. Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept. MSFC, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.

1947-, Katz Joseph, and United States. National Aeronautics and Space Administration., eds. Cellular structures in the flow over the flap of a two-element wing. [Washington, DC: National Aeronautics and Space Administration, 1997.

Walter, Frost, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Analysis of aerodynamic coefficients using gust gradient data: Spanwise turbulence effects on airplane response. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

R, Walsh Kevin, and NASA Dryden Flight Research Center., eds. Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack: Contract NAS 3-26617. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

R, Walsh Kevin, and NASA Dryden Flight Research Center., eds. Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack: Contract NAS 3-26617. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

G, Steenken W., and Hugh L. Dryden Flight Research Center., eds. Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.