Books on the topic 'Wind tunnel tests'
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Ajay, Kumar, Kegelman Jerome T, and United States. National Aeronautics and Space Administration., eds. The Langley wind tunnel enterprise. [Washington, DC: National Aeronautics and Space Administration, 1998.
Find full textAjay, Kumar, Kegelman Jerome T, and United States. National Aeronautics and Space Administration., eds. The Langley wind tunnel enterprise. [Washington, DC: National Aeronautics and Space Administration, 1998.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Quality assessment for wind tunnel testing. Neuilly-sur-Seine, France: AGARD, 1994.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Quality assessment for wind tunnel testing. Neuilly-sur-Seine: AGARD, 1994.
Find full textMacKinnon, A. Wind tunnel tests on a variable camber wing. Cranfield, Bedford, England: College of Aeronautics, Cranfield University, 1993.
Find full textGalway, R. D. The IAR High Reynolds Number Two-Dimensional Test Facility - a description of equipment and procedures common to most 2-D airfoil tests. Ottawa, Ont: National Research Council Canada, Institute for Aerospace Research, 1990.
Find full textGalway, R. D. The IAR high Reynolds number two-dimensional test facility - a description of equipment and procedures common to most 2-D airfoil tests. Ottawa: National Research Council of Canada, Institute for Aerospace Research, 1990.
Find full textCenter, Lewis Research, and United States. National Aeronautics and Space Administration., eds. Flow field surveys of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1993 test). [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Find full textKelly, Abeyounis William, and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textKelly, Abeyounis William, and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textK, Abeyounis W., and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textA, Kilgore Robert, Moore Deborah L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Cryogenic wind tunnels: A comprehensive, annotated bibliography. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Find full textA, Kilgore Robert, Cole Karen L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Cryogenic wind tunnels: A selected, annotated bibliography. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textBritcher, Colin P. Applications of magnetic suspension technology to large scale facilities: Progress, problems and promises. [Washington, DC: National Aeronautics and Space Administration, 1997.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textBritcher, Colin P. Application of magnetic suspension and balance systems to ultra-high Reynolds number facilities. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Find full textA, Laub James, and Ames Research Center, eds. NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.
Find full textMabey, Dennis G. Further buffeting tests in a cryogenic wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textMabey, D. G. Further buffeting tests in a cryogenic wind tunnel. London: HMSO, 1991.
Find full textR, Curry Monroe, Arrington E. Allen, United States. National Aeronautics and Space Administration., NASA Glenn Research Center, American Institute of Aeronautics and Astronautics., and Aerospace Sciences Meeting & Exhibit (39th : 2001 : Reno, Nev.), eds. Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textR, Curry Monroe, Arrington E. Allen, United Stares. National Aeronautics and Space Administration., NASA Glenn Research Center, American Institute of Aeronautics and Astronautics., and Aerospace Sciences Meeting & Exhibit (39th : 2001 : Reno, Nev.), eds. Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textR, Curry Monroe, Arrington E. Allen, United Stares. National Aeronautics and Space Administration., NASA Glenn Research Center, American Institute of Aeronautics and Astronautics., and Aerospace Sciences Meeting & Exhibit (39th : 2001 : Reno, Nev.), eds. Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textR, Curry Monroe, Arrington E. Allen, United States. National Aeronautics and Space Administration., NASA Glenn Research Center, American Institute of Aeronautics and Astronautics., and Aerospace Sciences Meeting & Exhibit (39th : 2001 : Reno, Nev.), eds. Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textBaumeister, Kenneth J. Reverberation effects on directionality and response of stationary monopole and dipole sources in a wind tunnel. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.
Find full textCenter, Langley Research, ed. A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textCenter, Langley Research, ed. A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textCenter, Langley Research, ed. A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textButtrill, Carey S. Aeroservoelastic simulation of an active flexible wing wind tunnel model. Hampton, Va: Langely Research Center, 1996.
Find full textA, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textA, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textA, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textA, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textMineck, Raymond E. Wind-tunnel investigation of aerodynamic efficiency of three planar elliptical wings with curvature of quarter-chord line. Hampton, Va: Langley Research Center, 1993.
Find full textMirick, Paul H. Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing. Hampton, Va: Langley Research Center, 1990.
Find full textAllen, Kilgore W., and Langley Research Center, eds. Microcomputer based controller for the Langley 0.3-meter Transonic Cryogenic Tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textT, Lund, Rote Donald, and Langley Research Center, eds. High-lift flight tunnel: Phase II report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.
Find full textT, Lund, Rote Donald, and Langley Research Center, eds. High-lift flight tunnel: Phase II report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.
Find full textRizkalla, Oussama F. High pressure hypervelocity electrothermal wind tunnel performance study and subscale tests. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.
Find full textNewton, James E. Study of ice accretion on icing wind tunnel components. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.
Find full textLarson, Terry J. Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.
Find full textR, Moes Timothy, Siemers Paul M, and Dryden Flight Research Facility, eds. Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.
Find full textWieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textWieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textWieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textWieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textAllen, Arrington E., American Institute of Aeronautics and Astronautics., NASA Glenn Research Center, and Aerospace Sciences Meeting & Exhibit (36th : 1998 : Reno, Nev.), eds. Aerodynamic calibration of the NASA Lewis icing research tunnel (1997 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textCenter, Langley Research, and United States. National Aeronautics and Space Administration, eds. Aeroservoelastic testing of free flying wind tunnel models. Hampton, Virginia: National Aeronautics and Space Administration, Langley Research Center, 2013.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Wall interference, support interference and flow field measurements. Neuilly sur Seine, France: AGARD, 1994.
Find full textAdvisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium,, ed. Wall interference, support interference and flow field measurements: Papers presented and discussions recorded at the 73rd Fluid Dynamics Panel Symposium held in Brussels, Belgium, 4th-7th October 1993. Neuilly sur Seine: Agard, 1994.
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