Books on the topic 'Wind tunnel tests'

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.

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.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Quality assessment for wind tunnel testing. Neuilly-sur-Seine, France: AGARD, 1994.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Quality assessment for wind tunnel testing. Neuilly-sur-Seine: AGARD, 1994.

MacKinnon, A. Wind tunnel tests on a variable camber wing. Cranfield, Bedford, England: College of Aeronautics, Cranfield University, 1993.

Galway, 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.

Galway, 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.

Center, 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.

Kelly, 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.

Kelly, 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.

K, 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.

A, 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.

A, 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.

United 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.

Britcher, Colin P. Applications of magnetic suspension technology to large scale facilities: Progress, problems and promises. [Washington, DC: National Aeronautics and Space Administration, 1997.

United 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.

Britcher, Colin P. Application of magnetic suspension and balance systems to ultra-high Reynolds number facilities. [Washington, D.C: National Aeronautics and Space Administration, 1996.

A, 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.

Mabey, Dennis G. Further buffeting tests in a cryogenic wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Mabey, D. G. Further buffeting tests in a cryogenic wind tunnel. London: HMSO, 1991.

R, 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.

R, 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.

R, 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.

R, 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.

Baumeister, 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.

Center, 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.

Center, 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.

Center, 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.

Buttrill, Carey S. Aeroservoelastic simulation of an active flexible wing wind tunnel model. Hampton, Va: Langely Research Center, 1996.

A, 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.

A, 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.

A, 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.

A, 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.

Mineck, 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.

Mirick, Paul H. Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing. Hampton, Va: Langley Research Center, 1990.

Allen, 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.

T, 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.

T, 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.

Rizkalla, Oussama F. High pressure hypervelocity electrothermal wind tunnel performance study and subscale tests. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.

Newton, James E. Study of ice accretion on icing wind tunnel components. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Larson, 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.

R, 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.

Wieseman, 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.

Wieseman, 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.

Wieseman, 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.

Wieseman, 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.

Allen, 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.

Center, 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.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Wall interference, support interference and flow field measurements. Neuilly sur Seine, France: AGARD, 1994.

Advisory 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.