Книги з теми "Aerodynamic angle"
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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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаMatsuo, N. Aerodynamic characteristics of general aviation at high angle of attack with the propeller slipstream. Washington DC: National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаKlein, 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.
Знайти повний текст джерелаKlein, Vladislav. Aerodynamic parameters of high-angle-of-attack research vehicle (Harv) estimated from flight data. Hampton, Va: National Aeronautics and Space Administration, 1990.
Знайти повний текст джерелаCenter, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Знайти повний текст джерелаCenter, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Знайти повний текст джерелаCenter, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Знайти повний текст джерелаCenter, Ames Research, ed. Two-dimensional high-lift aerodynamic optimization using neural networks. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.
Знайти повний текст джерелаBjarke, 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.
Знайти повний текст джерелаBjarke, 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.
Знайти повний текст джерелаIsogai, Koji. Numerical simulation of dynamic stall of NACA0012 airfoil oscillating near static stall angle using the Navier-Stokes equations. Tokyo: National Aerospace Laboratory, 1992.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаPamadi, 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.
Знайти повний текст джерелаA, 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.
Знайти повний текст джерелаJulio, 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.
Знайти повний текст джерелаR, 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.
Знайти повний текст джерелаNdaona, 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.
Знайти повний текст джерелаNdaona, 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.
Знайти повний текст джерелаNdaona, 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.
Знайти повний текст джерелаNdaona, 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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаPiziali, 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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаM, 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.
Знайти повний текст джерелаK, 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.
Знайти повний текст джерелаOld 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.
Знайти повний текст джерелаOld 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.
Знайти повний текст джерелаWhipple, 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.
Знайти повний текст джерелаHahne, 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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаE, 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.
Знайти повний текст джерелаCatlin, 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.
Знайти повний текст джерелаCatlin, 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.
Знайти повний текст джерелаL, 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.
Знайти повний текст джерелаL, 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.
Знайти повний текст джерелаL, 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.
Знайти повний текст джерелаGeorge 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.
Знайти повний текст джерела1947-, 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.
Знайти повний текст джерелаWalter, 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.
Знайти повний текст джерелаR, 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.
Знайти повний текст джерелаR, 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.
Знайти повний текст джерелаG, 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.
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