Books on the topic 'Aerodynamic calculation'

Raithby, G. D. Calculation of subsonic aerodynamic flows, the de Havilland Aircraft of Canada, Limited, Downsview, Ont., September 2-4, 1986. Downsview, Ont: De Havilland Aircraft of Canada, Ltd, 1986.

Mavriplis, Dimitri J. Unstructured mesh algorithms for aerodynamic calculations. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1992.

Lan, C. Edward. Calculation of aerodynamic characteristics at high angles of attack for airplane configurations: Semi-annual status report on NASA grant NAG 1-635, August 1, 1986 - January 31, 1987. Lawrence, Kan: Flight Research Laboratory, the University of Kansas Center for Research, Inc., 1987.

Barger, Raymond L. On minimizing the number of calculations in design-by-analysis codes. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Ueda, Tetsuhiko. Unsteady aerodynamic calculations for general configurations by the doublet-point method. Tokyo, Japan: National Aerospace Laboratory, 1991.

Baysal, Oktay. Navier-Stokes calculations of scramjet-nozzle-afterbody flowfields. Norfolk, Va: Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University Research Foundation, 1991.

Baysal, Oktay. Navier-Stokes calculations of scramjet-nozzle-afterbody flowfields. Norfolk, Va: Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University Research Foundation, 1991.

Quinn, Robert D. Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Quinn, Robert D. Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Quinn, Robert D. Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation. Moffett Field, Calif: Ames Research Center, 1990.

Chislennyĭ raschet dvumernogo sverkhzvukovogo potoka gaza v ploskikh kanalakh. Moskva: Vychislitelʹnyĭ t͡s︡entr AN SSSR, 1986.

Lu, Shuquan. TDLM--a transonic doublet lattice method for 3D potential unsteady transonic flow calculation. Köhn: Deutsche Forschungsanstaltfür Luft- und Raumfahrt, 1992.

Scott, Robert C. A method of predicting quasi-steady aerodynamics for flutter analysis of high speed vehicles using steady CFD calculations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Yamamoto, Y. Some numerical calculations by using linear classical sonic theories approached from sub- or supersonic speeds. Washington, DC: National Aeronautics and Space Administration, 1987.

Thomas, Randy L. Calculating parachute descent rates: For high power rocket recovery applications : a technical treatise and manual of instruction. Fairbanks, Alaska (139 Kelsan Way, Fairbanks 99709): Paratech Parachutes, 1990.

Kantelis, John P. Calculations of axisymmetric vortex sheet roll-up using a panel and a filament model. Cambridge, Mass: Fluid Dynamics Research Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1986.

Theory of transonic astrophysical flows. Singapore: World Scientific, 1990.

Baysal, Oktay. Navier-Stokes calculations of transonic flows past cavities. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Baysal, Oktay. Navier-Stokes calculations of transonic flows past cavities. Hampton, Va: Langley Research Center, 1989.

Baysal, Oktay. Navier-Stokes calculations of transonic flows past cavities. Norfolk, Va: Old Dominion University Research Foundation, 1988.

Baysal, Oktay. Navier-Stokes calculations of transonic flows past cavities. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Schmidt, James F. Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors: User's manual. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Wood, William A. Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Krasnov, N. F. Aerodynamics: Fundamentals of Theory, Aerodynamics of an Airfoil and Wing; Methods of Aerodynamic Calculation. Imported Pubn, 1986.

Cebeci, Tuncer. An Engineering Approach to the Calculation of Aerodynamic Flows. Horizons Pub, 1999.

Cebeci, Tuncer. An Engineering Approach to the Calculation of Aerodynamic Flows. Springer, 1999.

A loudness calculation procedure applied to shaped sonic booms. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Calculation of non-stationary aerodynamic forces in the near sonic range. Washington, DC: National Aeronautics and Space Administration, 1988.

United States. National Aeronautics and Space Administration., ed. Calculation of non-stationary aerodynamic forces in the near sonic range. Washington, DC: National Aeronautics and Space Administration, 1988.

Calculation of aerodynamic characteristics of airplane configurations at high angles of attack. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Calculation of aerodynamic characteristics of airplane configurations at high angles of attack. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Roskam, Jan. Airplane Design Part VI : Preliminary Calculation of Aerodynamic Thrust and Power Characteristics. Design Analysis & Research, 2000.

1935-, Lan C. Edward, and United States. National Aeronautics and Space Administration., eds. Calculation of aerodynamic characteristics of airplane configurations at high angles of attack: Final report. Lawrence, Kan: Flight Research Laboratory, University of Kansas Center for Research, Inc., 1988.

Calculation of aerodynamic heat transfer for blunt-nosed thin wings at different angles of attack at supersonic speeds. Washington, DC: National Aeronautics and Space Administration, 1988.

V, Sankewitsch, and Langley Research Center, eds. Calculation of flight vibration levels of the AH-1G helicopter and correlation with existing flight vibration measurements. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

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.

Jing-Biau, Tseng, and United States. National Aeronautics and Space Administration., eds. Calculation of aerodynamic characteristics at high angles of attack for airplane configurations: Semi-annual status report on NASA grant NAG 1-635, August 1, 1986 - January 31, 1987. Lawrence, Kan: Flight Research Laboratory, the University of Kansas Center for Research, Inc., 1987.

Zuliani, Gary L. Aerodynamic flow calculations using finite-differences and multigrid. 2004.

Unstructured and adaptive mesh algorithms for aerodynamic calculations. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1992.

Center, Langley Research, ed. Unsteady transonic flow calculations for wing-fuselage configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

United States. National Aeronautics and Space Administration, ed. Vectorizable multigrid algorithms for transonic flow calculations. [Washington, D.C.?: National Aeronautics and Space Administration, 1985.

Dignan, Jay. Simulation of flexible aircraft using real time aerodynamic calculations. 2005.

1936-, Kawamura Takaichi, Bencze Daniel P, and Ames Research Center, eds. Calculation of external-internal flow fields for mixed-compression inlets. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Calculation of external-internal flow fields for mixed-compression inlets. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

1936-, Kawamura Takaichi, Bencze Daniel P, and Ames Research Center, eds. Calculation of external-internal flow fields for mixed-compression inlets. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Unsteady transonic flow calculations for interfering lifting surface configurations. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

W, Iliff Kenneth, and NASA Dryden Flight Research Center., eds. Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 2000.

W, Iliff Kenneth, and NASA Dryden Flight Research Center., eds. Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 2000.

Kent, Rockaway J., and United States. National Aeronautics and Space Administration., eds. Aerodynamic calculations related to tethered sub-satellite experiments: Final report. Nashville, TN: Vanderbilt University, School of Engineering, Dept of Mechanical Engineering, 1991.

Local Exhaust Ventilation: Aerodynamic Processes and Calculations of Dust Emissions. Taylor & Francis Group, 2015.