Books on the topic 'Wind-pressure Measurement'

1961-, Streluk Angella, ed. Wind and air pressure. Oxford: Heinemann Library, 2008.

Angella, Streluk, ed. Wind and air pressure. Oxford: Heinemann Library, 2003.

Moshasrov, V. Luminescent pressure sensors in aerodynamic experiments. Zhukovsky, Russia : Central Aerohydrodynamic Institute (TsAGI): CWA 22 Corporation, 1998.

Smith, Stewart Ellis. An instrument for measuring turbulence during wind erosion. Perth, W.A: Division of Environmental Science, Murdoch University, 1994.

Plentovich, Elizabeth B. Orifice-induced pressure error studies in Langley 7- by 10-foot High-Speed Tunnel. Washington: NASA, 1986.

Mineck, Raymond E. Steady and periodic pressure measurements on a generic helicopter fuselage model in the presence of a rotor. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

Cowperthwaite, N. A. Full scale and wind tunnel surface pressure measurements on the T.R.R.L. spray dispersion programme vehicles. Cranfield, U.K: College of Aeronautics, Cranfield Institute of Technology, 1987.

Chapman, John J. A hybrid electronically scanned pressure module for cryogenic environments. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Chapman, John J. A hybrid electronically scanned pressure module for cryogenic environments. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Mineck, 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. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Barna, 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. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Schuster, D. M. Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

Hoffenberg, R. Wake measurements in a strong adverse pressure gradient. [Washington, DC: National Aeronautics and Space Administration, 1995.

Hoffenberg, R. Wake measurements in a strong adverse pressure gradient. [Washington, DC: National Aeronautics and Space Administration, 1995.

Igoe, William B. Analysis of fluctuating static pressure measurements in the National Transonic Facility. Hampton, Va: Langley Research Center, 1996.

Martin, Colin A. Surface pressure measurements on the wing of a wind tunnel model during steady rotation. Melbourne, Australia: Aeronautical Research Laboratory, 1991.

Eckstrom, Clinton V. Measurements of unsteady pressure and structural response for an elastic supercritical wing. Hampton: National Aeronautics and Space Administration, Langley Research Center, 1994.

Eckstrom, Clinton V. Measurements of unsteady pressure and structural response for an elastic supercritical wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Eckstrom, Clinton V. Measurements of unsteady pressure and structural response for an elastic supercritical wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Holland, Scott D. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Garry, 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. Cranfield [U.K.]: College of Aeronautics, Cranfield Institute of Technology, 1987.

Center, Langley Research, ed. Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Wind and Air Pressure (Measuring the Weather/ 2nd Edition). Heinemann, 2007.

- and NASA Glenn Research Center, eds. Pressure probe designs for dynamic pressure measurements in a supersonic flow field. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Overview of the 1989 Wind Tunnel Calibration Workshop. Washington, DC: National Aeronautics and Space Administration, Scientific and Technical Information Program, 1993.

Streluk, Angella, and Alan Rodgers. Wind and Air Pressure (Rodgers, Alan, Measuring the Weather.). Heinemann, 2002.

K, Puram Chith, Upchurch Billy T, and United States. National Aeronautics and Space Administration., eds. Optimization of measurements with pressure sensitive paints. [Washington, DC]: NASA, 1995.

L, Schultz Larry, and John F. Kennedy Space Center., eds. Comparison of analytical methods for calculation of wind loads. [Kennedy Space Center, FL]: National Aeronautics and Space Administration, John F. Kennedy Space Center, 1989.

A, Rivera José, and Langley Research Center, eds. Sidewall Mach number distributions for the NASA Langley Transonic Dynamics Tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

M, 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. [Washington, DC: National Aeronautics and Space Administration, 1994.

B, 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. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Infomraton Branch, 1986.

B, 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. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Infomraton Branch, 1986.

United States. National Aeronautics and Space Administration., ed. Application of pressure sensitive paint in hypersonic flows. [Washington, DC]: National Aeronautics and Space Administration, 1995.

G, 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. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.

G, 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. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.

Development of a variational SEASAT data analysis technique: Final report. [Washington, DC: National Aeronautics and Space Administration, 1986.

W, Edwards John, and Langley Research Center, eds. Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

W, 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. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Ed, 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. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Description and assessment of a new optical pressure measurement system (OPMS) demonstrated in the high speed wind tunnel of DLR in Göttingen. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrhart, 1992.

Joseph, 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. [Washington, DC: National Aeronautics and Space Administration, 1996.

A, Heelis Rodney, and United States. National Aeronautics and Space Administration., eds. A satellite anemometer: Final report for NASA grant NAGW-2534. [Washington, D.C: National Aeronautics and Space Administration, 1995.

A, Heelis Rodney, and United States. National Aeronautics and Space Administration., eds. A satellite anemometer: Final report for NASA grant NAGW-2534. [Washington, D.C: National Aeronautics and Space Administration, 1995.

A, Heelis Rodney, and United States. National Aeronautics and Space Administration., eds. A satellite anemometer: Final report for NASA grant NAGW-2534. [Washington, D.C: National Aeronautics and Space Administration, 1995.

J, 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. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

Center, Lewis Research, ed. Experimental study of boundary layer behavior in a simulated low pressure turbine. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Center, Lewis Research, ed. Experimental study of boundary layer behavior in a simulated low pressure turbine. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Jet 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. Pasadena, Calif: Jet Propulsion Laboratory, California Institute of Technology, 1985.

Jet 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. Pasadena, Calif: Jet Propulsion Laboratory, California Institute of Technology, 1985.

Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel: Report on the modified D.S.M.A. design. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.