Books on the topic 'Wind-pressure Measurement'
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E, Simley, Pao L. Y, and National Renewable Energy Laboratory (U.S.), eds. LIDAR wind speed measurement analysis and feed-forward blade pitch control for load mitigation in wind turbines: January 2010 - January 2011. National Renewable Energy Laboratory, 2011.
Find full text- and NASA Glenn Research Center, eds. Pressure probe designs for dynamic pressure measurements in a supersonic flow field. National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textCenter, Langley Research, ed. Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textK, Puram Chith, Upchurch Billy T, and United States. National Aeronautics and Space Administration., eds. Optimization of measurements with pressure sensitive paints. NASA, 1995.
Find full textL, Schultz Larry, and John F. Kennedy Space Center., eds. Comparison of analytical methods for calculation of wind loads. National Aeronautics and Space Administration, John F. Kennedy Space Center, 1989.
Find full textMoshasrov, V. Luminescent pressure sensors in aerodynamic experiments. CWA 22 Corporation, 1998.
Find full textSmith, Stewart Ellis. An instrument for measuring turbulence during wind erosion. Division of Environmental Science, Murdoch University, 1994.
Find full textA, Rivera José, and Langley Research Center, eds. Sidewall Mach number distributions for the NASA Langley Transonic Dynamics Tunnel. National Aeronautics and Space Administration, Langley Research Center, 2001.
Find full textB, Gloss Blair, and United States. National Aeronautics and Space Administration., eds. Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel. National Aeronautics and Space Administration, Scientific and Technical Infomraton Branch, 1986.
Find full textPlentovich, Elizabeth B. Orifice-induced pressure error studies in Langley 7- by 10-foot High-Speed Tunnel. NASA, 1986.
Find full textB, Gloss Blair, and United States. National Aeronautics and Space Administration., eds. Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel. National Aeronautics and Space Administration, Scientific and Technical Infomraton Branch, 1986.
Find full textM, Helland Stephen, and United States. National Aeronautics and Space Administration., eds. Improved pressure measurement system for calibration of the NASA LeRC 10x10 supersonic wind tunnel. National Aeronautics and Space Administration, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. Application of pressure sensitive paint in hypersonic flows. National Aeronautics and Space Administration, 1995.
Find full textMineck, Raymond E. Steady and periodic pressure measurements on a generic helicopter fuselage model in the presence of a rotor. National Aeronautics and Space Administration, Langley Research Center, 2000.
Find full textChapman, John J. A hybrid electronically scanned pressure module for cryogenic environments. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textChapman, John J. A hybrid electronically scanned pressure module for cryogenic environments. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textCowperthwaite, N. A. Full scale and wind tunnel surface pressure measurements on the T.R.R.L. spray dispersion programme vehicles. College of Aeronautics, Cranfield Institute of Technology, 1987.
Find full textG, Rehm Ronald, National Institute of Standards and Technology (U.S.), and Building and Fire Research Laboratory (U.S.), eds. An efficient large eddy simulation algorithm for computational wind engineering: Application to surface pressure computations on a single building. U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.
Find full textG, Rehm Ronald, National Institute of Standards and Technology (U.S.), and Building and Fire Research Laboratory (U.S.), eds. An efficient large eddy simulation algorithm for computational wind engineering: Application to surface pressure computations on a single building. U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.
Find full textCenter, Langley Research, ed. Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel. National Aeronautics and Space Administration, Langley Research Center, 2013.
Find full textMineck, Raymond E. Application of an unstructured grid Navier-Stokes solver to a generic helicopter body: Comparison of unstructured grid results with structured grid results and experimental results. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textW, Edwards John, and Langley Research Center, eds. Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textEd, Pendleton, and Langley Research Center, eds. A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textW, Cazier F., Wynne Eleanor C, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textJoseph, Katz, Ross James, and United States. National Aeronautics and Space Administration., eds. Final report on study of organized structures in the post-stall flow over wings. National Aeronautics and Space Administration, 1996.
Find full textA, Heelis Rodney, and United States. National Aeronautics and Space Administration., eds. A satellite anemometer: Final report for NASA grant NAGW-2534. National Aeronautics and Space Administration, 1995.
Find full textA, Heelis Rodney, and United States. National Aeronautics and Space Administration., eds. A satellite anemometer: Final report for NASA grant NAGW-2534. National Aeronautics and Space Administration, 1995.
Find full textA, Heelis Rodney, and United States. National Aeronautics and Space Administration., eds. A satellite anemometer: Final report for NASA grant NAGW-2534. National Aeronautics and Space Administration, 1995.
Find full textJ, Yuhas Andrew, and NASA Dryden Flight Research Center., eds. F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack: Contract NAS 3-26617. National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.
Find full textCenter, Lewis Research, ed. Experimental study of boundary layer behavior in a simulated low pressure turbine. National Aeronautics and Space Administration, Lewis Research Center, 1998.
Find full textCenter, Lewis Research, ed. Experimental study of boundary layer behavior in a simulated low pressure turbine. National Aeronautics and Space Administration, Lewis Research Center, 1998.
Find full textJet Propulsion Laboratory (U.S.) and Nova University, eds. Air-sea interaction with SSM/I and altimeter: Report of the NASA Ocean Energy Fluxes Science Working Group. Jet Propulsion Laboratory, California Institute of Technology, 1985.
Find full textJet Propulsion Laboratory (U.S.) and Nova University, eds. Air-sea interaction with SSM/I and altimeter: Report of the NASA Ocean Energy Fluxes Science Working Group. Jet Propulsion Laboratory, California Institute of Technology, 1985.
Find full textBarna, P. S. Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel: Progress report on the D.S.M.A. design. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textCenter, Langley Research, ed. Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel: Progress report on the D.S.M.A. design. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textSchuster, D. M. Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel. National Aeronautics and Space Administration, Langley Research Center, 2001.
Find full textHoffenberg, R. Wake measurements in a strong adverse pressure gradient. National Aeronautics and Space Administration, 1995.
Find full textHoffenberg, R. Wake measurements in a strong adverse pressure gradient. National Aeronautics and Space Administration, 1995.
Find full textIgoe, William B. Analysis of fluctuating static pressure measurements in the National Transonic Facility. Langley Research Center, 1996.
Find full textMartin, Colin A. Surface pressure measurements on the wing of a wind tunnel model during steady rotation. Aeronautical Research Laboratory, 1991.
Find full textEckstrom, Clinton V. Measurements of unsteady pressure and structural response for an elastic supercritical wing. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textEckstrom, Clinton V. Measurements of unsteady pressure and structural response for an elastic supercritical wing. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textEckstrom, Clinton V. Measurements of unsteady pressure and structural response for an elastic supercritical wing. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textHolland, Scott D. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textCenter, Langley Research, ed. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textGarry, Kevin P. A summary of the scale model wind tunnel measurements and full scale surface pressure tests on the Leyland T45 and DAF3300 vehicles used for the TRRL spray dispersion programme. College of Aeronautics, Cranfield Institute of Technology, 1987.
Find full textOverview of the 1989 Wind Tunnel Calibration Workshop. National Aeronautics and Space Administration, Scientific and Technical Information Program, 1993.
Find full textStreluk, Angella, and Alan Rodgers. Wind and Air Pressure (Rodgers, Alan, Measuring the Weather.). Heinemann, 2002.
Find full textDevelopment of a variational SEASAT data analysis technique: Final report. National Aeronautics and Space Administration, 1986.
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