Books on the topic 'Aerodynamic pressure'
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K, Notestine Kristopher, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Aerodynamic pressure and heating-rate distributions in tile gaps around chine regions with pressure gradients at a Mach number of 6.6. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textMoshasrov, V. Luminescent pressure sensors in aerodynamic experiments. CWA 22 Corporation, 1998.
Find full textH, Ricketts Rodney, Hess R. W, and Langley Research Center, eds. Recent transonic unsteady pressure measurements at the NASA Langley Research Center. National Aeronautics and Space Administration, Langley Research Center, 1985.
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 textE, Mineck Raymond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Find full textNemec, Marian. Aerodynamic computations using the convective upstream split pressure scheme with local preconditioning. Dept. of Aerospace Science and Engineering, University of Toronto, 1998.
Find full textNemec, Marian. Aerodynamic computations using the convective upstream split pressure scheme with local preconditioning. National Library of Canada, 1998.
Find full textLabrujere, Th E. Correction for wall interference in a solid-wall wind tunnel using sparse measured boundary conditions. National Aerospace Laboratory, 1989.
Find full textUnited States. National Aeronautics and Space Administration., ed. IPAC--Inlet Performance Analysis Code. National Aeronautics and Space Administration, 1997.
Find full textUnited States. National Aeronautics and Space Administration., ed. IPAC--Inlet Performance Analysis Code. National Aeronautics and Space Administration, 1997.
Find full textUnited States. National Aeronautics and Space Administration., ed. IPAC--Inlet Performance Analysis Code. National Aeronautics and Space Administration, 1997.
Find full textS, Hultberg Randy, Martin Colin A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Find full textCenter, Ames Research, ed. Improved two-equation k - [omega] turbulence models for aerodynamic flows. National Aeronautics and Space Administration, Ames Research Center, 1992.
Find full textCenter, Ames Research, ed. Improved two-equation k - [omega] turbulence models for aerodynamic flows. National Aeronautics and Space Administration, Ames Research Center, 1992.
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 textWing, David J. Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textEmre, Ilgin Hüseyin, ed. Tall buildings: Structural systems and aerodynamic form. Routledge, Taylor & Francis Group, 2014.
Find full textCenter, Ames Research, and U.S. Army Aviation and Troop Command., eds. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command, 1994.
Find full textCenter, Ames Research, and U.S. Army Aviation and Troop Command., eds. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command, 1994.
Find full textCenter, Ames Research, and U.S. Army Aviation and Troop Command., eds. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command, 1994.
Find full textPiziali, R. A. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. Ames Research Center, 1994.
Find full textCenter, Ames Research, and U.S. Army Aviation and Troop Command., eds. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command, 1994.
Find full textK. B. M. Q. Zaman. Some observations on transitory stall in conical diffusers. Lewis Research Center, 1989.
Find full textUnited States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Semi-annual report #4, January-June 1993. CSTAR - Center for Space Transportation and Applied Research, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Final report, June 1991 - June 1994. Center for Space Transportation and Applied Research, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Semi-annual report #2, January - June 1992. University of Tennessee Space Institute, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system. National Aeronautics and Space Administration, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Semi-annual report #2, January - June 1992. University of Tennessee Space Institute, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Semi-annual report #3, July - December 1992. University of Tennessee Space Institute, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Semi-annual report #4, January-June 1993. CSTAR - Center for Space Transportation and Applied Research, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system. National Aeronautics and Space Administration, 1994.
Find full textUnited 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. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
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 textMoes, Timothy R. In-flight investigation of shuttle tile pressure orifice installations. Ames Research Center, 1990.
Find full textR, Meyer Robert, and Ames Research Center, eds. In-flight investigation of shuttle tile pressure orifice installations. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textMoes, Timothy R. In-flight investigation of shuttle tile pressure orifice installations. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textSiemers, Paul M. Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel. National Aeronautics and Space Administration, Langley Research Center, 1986.
Find full textApplin, Zachary T. Pressure distributions from subsonic tests of a NACA 0012 semispan wing model. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textApplin, Zachary T. Pressure distributions from subsonic tests of a NACA 0012 semispan wing model. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textGuerrera, Michael H. Laser anemometry and pressure measurements in the endwall region of an annular turbine cascade utilizing a pressurized aerodynamic window. Naval Postgraduate School, 1996.
Find full textSiemers, Paul M. Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel. National Aeronautics and Space Administration, Langley Research Center, 1986.
Find full text1947-, Katz Joseph, and United States. National Aeronautics and Space Administration., eds. Cellular structures in the flow over the flap of a two-element wing. National Aeronautics and Space Administration, 1997.
Find full textLee, Harvey Shui-Hong. Assessment of potential aerodynamic effects on personnel and equipment in proximity to high-speed train operations: Safety of high-speed ground transportation systems. U.S. Dept. of Transportation, Federal Railroad Administration, Office of Research and Development, 1999.
Find full textJenkins, Renaldo. Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-Meter Transonic Cryogenic Tunnel. Langley Research Center, 1988.
Find full textS, Hill Aquilla, Ray Edward J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter Transonic Cryogenic Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textHallissy, James B. Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow. Langley Research Center, 1989.
Find full textKontos, K. B. Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems. National Aeronautics and Space Administration, 1996.
Find full textKontos, K. B. Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems. National Aeronautics and Space Administration, 1996.
Find full textKontos, K. B. Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems. National Aeronautics and Space Administration, 1996.
Find full textKontos, K. B. Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems. National Aeronautics and Space Administration, 1996.
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