Libros sobre el tema "Wind tunnel cascade test"
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Norris, R. B. The flying wind tunnel. New York: AIAA, 1989.
Buscar texto completoB, Kelley P. y United States. National Aeronautics and Space Administration, eds. Wind tunnel test IA300 analysis and results. Huntsville, AL: Lockheed Missiles & Space Co., Huntsville Engineering Center, 1987.
Buscar texto completoK, Wailes W. y Ames Research Center, eds. Advanced recovery systems wind tunnel test report. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Buscar texto completoKeas, Paul. SOFIA II model telescope and wind tunnel test. [Moffett Field, Calif.]: NASA Ames Research Center, 1995.
Buscar texto completoBaydar, Adem. Hot-wire measurements of compressor blade wakes in a cascade wind tunnel. Monterey, California: Naval Postgraduate School, 1988.
Buscar texto completoKelly, Abeyounis William y Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Buscar texto completoK, Abeyounis W. y Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Buscar texto completoKelly, Abeyounis William y Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Buscar texto completoOhman, L. H. New transonic test sections for the NAE 5ftx5ft trisonic wind tunnel. Ottawa: National Aeronautical Establishment, 1990.
Buscar texto completoRandall, Peterson y Ames Research Center, eds. Shake test results of the MDHC test stand in the 40- by 80-foot wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.
Buscar texto completoL, Peterson Randall y Ames Research Center, eds. Shake test results of the MDHC test stand in the 40- by 80-foot wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.
Buscar texto completoA, Kennelly Robert y Ames Research Center, eds. Transonic wind tunnel test of a 14% thick oblique wing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Buscar texto completoGlynn, J. L. Space shuttle phase B wind tunnel model and test information. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Buscar texto completoAllen, Dale, Lorber Peter y Ames Research Center, eds. Wind tunnel test of a variable-diameter tiltrotor (VDTR) model. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.
Buscar texto completoCenter, Ames Research, ed. Analysis of the free-tip rotor wind-tunnel test results. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.
Buscar texto completoGlynn, J. L. Space shuttle Phase B wind tunnel test database: Summary report. Hampton, Va: Langley Research Center, 1988.
Buscar texto completoCenter, Ames Research, ed. Analysis of the free-tip rotor wind-tunnel test results. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.
Buscar texto completoKhadjavi, F. Two-dimensional test section with preadjusted adaptive walls for low speed wind tunnel. Stockholm: Royal Institute of Technology, Department of Aeronautics, 1987.
Buscar texto completoCenter, Langley Research, ed. Wall adjustment strategy software for use with the NASA Langley 0.3-meter transonic cryogenic tunnel adaptive wall test section. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Buscar texto completoHoad, Danny R. Rotor performance characteristics from an aeroacoustics helicopter wind-tunnel test program. Hampton, Va: Langley Research Center, 1986.
Buscar texto completoW, Elliott Joe, Orie Nettie M, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., United States. Army Aviation Systems Command. y Langley Research Center, eds. Rotor performance characteristics from an aeroacoustic helicopter wind-tunnel test program. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Buscar texto completoNational Research Council of Canada. y National Aeronautical Establishment (Canada), eds. New transonic test sections for the NAE 5ftx5ft trisonic wind tunnel. Ottawa: National Research Council Canada, 1990.
Buscar texto completoCapone, Francis J. The NASA Langley 16-Foot Transonic Tunnel: Historical overview, facility description, calibration, flow characteristics, and test capabilities. Hampton, Va: Langley Research Center, 1995.
Buscar texto completoMurray, Kenneth Douglas. Automation and extension of LDV measurements of off-design flow in a cascade wind tunnel. Monterey, Calif: Naval Postgraduate School, 1989.
Buscar texto completoAl-Saadi, Jassim A. Wall interference and boundary simulation in a transonic wind tunnel with a discretely slotted test section. Hampton, Va: Langley Research Center, 1993.
Buscar texto completoCenter, Langley Research, ed. The experimental verification of wall movement influence coefficients for an adaptive walled test section. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Buscar texto completoGalway, 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.
Buscar texto completoGalway, 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.
Buscar texto completoCenter, Lewis Research y 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.
Buscar texto completoA, Campbell William. Large scale advanced prop-fan (LAP) high speed wind tunnel test report. [Windsor Locks, CT]: Hamilton Standard Division, United Technologies Corporation, 1989.
Buscar texto completoR, Riley Donald y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Buscar texto completoR, Moes Timothy y Dryden Flight Research Facility, eds. Wind-tunnel development of an SR-71 aerospike rocket flight test configuration. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1996.
Buscar texto completoR, Moes Timothy y Dryden Flight Research Facility, eds. Wind-tunnel development of an SR-71 aerospike rocket flight test configuration. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1996.
Buscar texto completoCoe, Paul L. Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept. Hampton, Va: Langley Research Center, 1988.
Buscar texto completoR, Riley Donald y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. SOFIA, AFT cavities wind tunnel test: SOFIA II, final report : appendix E. [Washington, DC: National Aeronautics and Space Administration, 1994.
Buscar texto completoR, Riley Donald y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Buscar texto completoSprinkle, Danny R. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoSprinkle, Danny R. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoP, Davis Patricia y Langley Research Center, eds. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoSprinkle, Danny R. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoSprinkle, Danny R. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoSprinkle, Danny R. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoS, Hill Acquilla y United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Buscar texto completoC, Wilson John. Wind tunnel test results of a 1/8-scale fan-in-wing model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Buscar texto completoManuel, Gregory S. Effect of collector configuration on test section turbulence levels in an open-jet wind tunnel. Hampton, Va: Langley Research Center, 1992.
Buscar texto completoSchairer, Edward T. A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. Methods for scaling icing test conditions. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Buscar texto completoUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Computer simulation of a wind tunnel test section with discrete finite-length wall slots. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Buscar texto completoGoodyer, M. J. A swept wing panel in a low speed flexible walled test section. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
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