Books on the topic 'Aerodynamic load'

United States. National Aeronautics and Space Administration., ed. A characteristic method for calculating the generalized flat flutter aerodynamic forces. Washington, DC: National Aeronautics and Space Administration, 1988.

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Aircraft dynamic loads due to flow separation. Neuilly sur Seine, France: AGARD, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aircraft dynamic loads due to flow separation. Neuilly-sur-Seine: AGARD, 1990.

Pérez, Sergio Adrián. Sergio Adrián Pérez. Downsview, Ont: Institute for Aerospace Studies, University of Toronto, 1990.

Moshasrov, V. Luminescent pressure sensors in aerodynamic experiments. Zhukovsky, Russia : Central Aerohydrodynamic Institute (TsAGI): CWA 22 Corporation, 1998.

R, Burley James, Bare E. Ann, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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.

Wing, David J. Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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.

Lee, B. H. K. Forced oscillation of a two-dimensional airfoil with nonlinear aerodynamic loads. Ottawa: National Aeronautical Establishment, 1986.

Winebarger, Roger M. Loads and motions of an F-106B flying through thunderstorms. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Jack, King, Milligan Michael, Utility Wind Integration Group. Fall Technical Workshop, and National Renewable Energy Laboratory (U.S.), eds. Allocating variability and reserve requirements. Golden, Colo.]: National Renewable Energy Laboratory, 2011.

Jenkins, Jerald M. A summary of numerous strain-gage load calibrations on aircraft wings and tails in a technology format. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1997.

Yates, John E. Analysis of the surface load and radiated sound of a vibrating airfoil with application to the experiment of Brooks. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Joseph, Katz. Evaluation of an aerodynamic-load prediction method on an STOL fighter configuration. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

Chattopadhyay, Aditi. An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades. Hampton, Va: Langley Research Center, 1990.

Kerr, Patricia A. User's guide: Steady-state aerodynamic-loads program for shuttle TPS tiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Kerr, Patricia A. User's guide: Steady-state aerodynamic-loads program for shuttle TPS tiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Schreck, Scott J. Final report: IEA Wind Annex XX : HAWT aerodynamics and models from wind tunnel measurements. Golden, Colo: National Renewable Energy Laboratory, 2008.

Ning, N. A. CCBLADE documentation. Golden, CO: National Renewable Energy Laboratory, 2013.

Howe, Denis. Aircraft loading and structural layout. Reston, VA: American Institute of Aeronautics and Astronautics, 2004.

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.

Molenaar, David-Pieter. Cost-effective design and operation of variable speed wind turbines: Closing the gap between the control engineering and the wind engineering community. Delft, the Netherlands: Delft University Press, 2003.

Siemers, Paul M. Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

S, Hultberg Randy, Martin Colin A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Siemers, Paul M. Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

M, Bahm Catherine, Heinle Robert A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Determination of stores pointing error due to wing flexibility under flight load. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

United States. National Aeronautics and Space Administration, ed. An investigation of tip planform influence on the aerodynamic load characteristics of a semi-span, unswept wing and wing-tip. Lawrence, Kan: University of Kansas Center for Research, Inc., 1985.

Center, Ames Research, ed. An investigation of tip planform influence on the aerodynamic load characteristics of a semi-span, unswept wing and wing-tip. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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.

McMaster, Hal C. FAR 23 loads: Computer aided engineering for airplane loads to federal air regulations. [Wichita, Kan.] (7415 Tanglewood Ct., Wichita 67206): Aero Science Software, 1991.

Fisher, David F. F-18 High Alpha Research Vehicle surface pressures: Initial in-flight results and correlation with flow visualization and wind-tunnel data. Edwards, Calif: NASA Ames Resarch Center, Dryden Flight Research Facility, 1990.

W, Banks Daniel, Richwine David M, Dryden Flight Research Facility, and AIAA Applied Aeronautics Conference (8th : 1990 : Portland, Or.), eds. F-18 High Alpha Research Vehicle surface pressures: Initial in-flight results and correlation with flow visualization and wind-tunnel data. Edwards, Calif: NASA Ames Resarch Center, Dryden Flight Research Facility, 1990.

Moes, Timothy R. In-flight investigation of shuttle tile pressure orifice installations. Edwards, Calif: Ames Research Center, 1990.

R, Meyer Robert, and Ames Research Center, eds. In-flight investigation of shuttle tile pressure orifice installations. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

W, Banks Daniel, Richwine David M, Dryden Flight Research Facility, and AIAA Applied Aeronautics Conference ( 8th : 1990 : Portland, Oregon), eds. F-18 High Alpha Research Vehicle surface pressures: Initial in-flight results and correlation with flow visualization and wind-tunnel data. Edwards, Calif: NASA Ames Resarch Center, Dryden Flight Research Facility, 1991.

Fisher, David F. F-18 High Alpha Research Vehicle surface pressures: Initial in-flight results and correlation with flow visualization and wind-tunnel data. Edwards, Calif: NASA Ames Resarch Center, Dryden Flight Research Facility, 1990.

Moes, Timothy R. In-flight investigation of shuttle tile pressure orifice installations. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Dillenius, Marnix F. E. Improvements to the missile aerodynamic prediction code DEMON3. Hampton, Va: Langley Research Center, 1992.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Reduction of structural loads using the maneuver load control on the advanced fighter technology integration (AFTI)/F-111 mission adaptive wing. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

S, Pototzky Anthony, and Langley Research Center, eds. Rolling maneuver load alleviation using active controls. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

S, Pototzky Anthony, and Langley Research Center, eds. Rolling maneuver load alleviation using active controls. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Jankovsky, Robert S. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

G, Bousman William, and Ames Research Center, eds. Aerodynamic limitations of the UH-60A rotor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aircraft loads due to turbulence and their impact on design and certification. Neuilly sur Seine, France: AGARD, 1994.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aircraft loads due to turbulence and their impact on design and certification. Neuilly sur Seine, France: AGARD, 1994.

Baumann, Peter Helmut. Messung von aerodynamisch bedingten Modellverformungen im Windkanal mittels Moire-Interferometrie. Koln, Germany: DLR, 1994.