Books on the topic 'Low wind speed threshold'

Barlow, Jewel B. Low-speed wind tunnel testing. 3rd ed. New York: Wiley, 1999.

Simiu, Emil. Extreme wind distribution tails: A 'peaks over threshold' approach. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1995.

Bell, James H. Contraction design for small low-speed wind tunnels. Stanford, Calif: Stanford University, Department of Aeronautics and Astronautics, 1988.

Bell, J. H. Contraction design for small low-speed wind tunnels. [Washington, DC: National Aeronautics and Space Administration, 1988.

Simiu, Emil. Estimates of hurricane wind speeds by the 'peaks over threshold' method. Gaithersburg, MD: U.S. Department of Commerce, Technology Administration, National Institute of Standards and Technology, 1996.

Hughes, Christopher G. Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Hughes, Christopher G. Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Hughes, Christopher G. Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Watmuff, J. H. Design of a new contraction for the ARL low speed wind tunnel (U). Melbourne, Australia: Aeronautical Research Laboratories, 1986.

Dunham, Dana Morris. Low-speed wind-tunnel tests of single- and counter-rotation propellers. [s.l.]: National Aeronautics and Space Administration Scientific and Technical Information Branch, 1986.

Dunham, Dana Morris. Low-speed wind-tunnel tests of single- and counter-rotation propellers. Hampton, Va: Langley Research Center, 1986.

Goodyer, 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.

Goodyer, M. J. A swept wing panel in a low speed flexible walled test section. Hampton, Va: Langley Research Center, 1987.

Khadjavi, F. Two-dimensional test section with preadjusted adaptive walls for low speed wind tunnel. Stockholm: Royal Institute of Technology, Department of Aeronautics, 1987.

Ferris, James C. Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil. Hampton, Va: Langley Research Center, 1987.

Coe, Paul L. Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept. Hampton, Va: Langley Research Center, 1988.

Lance, Michael B. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Lance, Michael B. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. Hampton, Va: Langley Research Center, 1991.

Hunter, M. H. A guide to the DRA 13ft x 9ft low speed wind tunnel facility. Farnborough: Defence Research Agency, 1993.

Lines, I. G. The implications of dispersion in low wind speed conditions for quantified risk assessment. [Sudbury]: HSE Books, 1997.

Friedrichs, Reinhard. Die Durchsatzmesseinrichtung des Niedergeschwindigkeits-Windkanals der DFVLR in Braunschweig. Koln: DFVLR, 1988.

Cripps, M. N. The 13ft x 9ft low speed wind tunnel facility at DRA (Aerospace Division) Bedford (UK). London: HMSO, 1991.

Coe, Paul L. Low-speed wind-tunnel investigation of the flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration. Hampton, Va: Langley Research Center, 1990.

Catlin, Gregory M. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Catlin, Gregory M. Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Riley, Donald R. Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept. Hampton, Va: Langley Research Center, 1989.

Riley, Donald R. Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Riley, Donald R. Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Allen, Jerry M. Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Fears, Scott P. Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Ashill, P. R. A study of the flow around the leading edge of a highly-swept wing in a low-speed wind tunnel. Farnborough: Defence Research Agency, 1993.

Fears, Scott P. Low-speed wind-tunnel investigation of a porous forebody and nose strakes for yaw control of a multirole fighter aircraft. Hampton, Va: Langley Research Center, 1995.

Block, P. J. W. Directory and trends of noise generated by a propeller in a wake. Hampton, Va: Langley Research Center, 1986.

Scott, Samuel J. Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Brandon, Jay M. Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration. Hampton, Va: Langley Research Center, 1986.

Hahne, David E. Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

United States. National Aeronautics and Space Administration., ed. Integral method of wall interference correction in low-speed wind tunnels. Washington, DC: National Aeronautics and Space Administration, 1987.

A, Gazzaniga John, and United States. National Aeronautics and Space Administration., eds. Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack. [Washington, DC]: National Aeronautics and Space Administration, 1989.

A, Gazzaniga John, and United States. National Aeronautics and Space Administration., eds. Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack. [Washington, DC]: National Aeronautics and Space Administration, 1989.

A, Gazzaniga John, and United States. National Aeronautics and Space Administration., eds. Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Low-speed wind tunnel tests of two waverider configuration models. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

Low-speed wind tunnel tests of two waverider configuration models. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

E, Hahne David, Cockrell Charles E, and United States. National Aeronautics and Space Administration., eds. Low-speed wind tunnel tests of two waverider configuration models. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

E, Hahne David, Cockrell Charles E, and United States. National Aeronautics and Space Administration., eds. Low-speed wind tunnel tests of two waverider configuration models. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

United States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.

NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Britcher, Colin, and Drew Landman. Wind Tunnel Test Techniques: Design and Use of Low- and High-Speed Wind Tunnels. Academic Press, 2021.

L, Gentry Carl, Dunham Dana Morris, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed wind-tunnel tests of an advanced eight-bladed propeller. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.