Books on the topic 'NACA 0018'
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K, Takahashi R., Ames Research Center, and United States. Army Aviation Systems Command., eds. NACA 0015 wing pressure and trailing vortex measurements. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Find full textHeyd, Darrick Vaughn. Photodissociation of methyl bromide adsorbed on LiF(001), NaCl(001), and MgO(001). National Library of Canada = Bibliothèque nationale du Canada, 1997.
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 textRobert, Shaw, Newton James E, and United States. National Aeronautics and Space Administration., eds. Ice shapes and the resulting drag increase for a NACA 0012 airfoil. National Aeronautics and Space Administration, 1985.
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 textMcCroskey, W. J. A critical assessment of wind tunnel results for the NACA 0012 airfoil. National Aeronautics and Space Administration, Ames Research Center, 1987.
Find full textMineck, Raymond E. Effect of full-chord porosity on aerodynamic characteristics of the NACA 0012 airfoil. Langley Research Center, 1996.
Find full textA, Rivera José, and Langley Research Center, eds. Experimental flutter boundaries with unsteady pressure distributions for the NACA 0012 Benchmark Model. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textH, Bond Thomas, and United States. National Aeronautics and Space Administration., eds. Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil. National Aeronautics and Space Administration, 1992.
Find full textH, Bond Thomas, and United States. National Aeronautics and Space Administration., eds. Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil. National Aeronautics and Space Administration, 1992.
Find full textGreen, Lawrence L. Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels. Langley Research Center, 1991.
Find full textA, Newman Perry, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Find full textM, Bragg, Shin Jaiwon, and United States. National Aeronautics and Space Administration., eds. Helium bubble flow visualization of the spanwise separation on a NACA 0012 with simulated glaze ice. National Aeronautics and Space Administration, 1992.
Find full textM, Bragg, Shin J, and United States. National Aeronautics and Space Administration., eds. Helium bubble flow visualization of the spanwise separation on a NACA 0012 with simulated glaze ice. National Aeronautics and Space Administration, 1992.
Find full textG, Potapczuk Mark, and United States. National Aeronautics and Space Administration., eds. Numerical modeling of anti-icing systems and comparison to test results on a NACA 0012 airfoil. National Aeronautics and Space Administration, 1993.
Find full textH, Bond Thomas, and United States. National Aeronautics and Space Administration., eds. Results of an icing test on a NACA 0012 airfoil in the NASA Lewis Icing Research Tunnel. National Aeronautics and Space Administration, 1992.
Find full textF, Okuno Arthur, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textPoinsatte, Philip E. Heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Icing Research Tunnel. Lewis Research Center, 1990.
Find full textUnited States. National Aeronautics and Space Administration., ed. An experimental mapping of the flow field behind a glaze ice shape on a NACA 0012 airfoil. National Aeronautics and Space Administration, 1988.
Find full textUnited States. National Aeronautics and Space Administration., ed. Prediction of ice accretion on a swept NACA 0012 airfoil and and comparisons of flight test results. National Aeronautics and Space Administration, 1992.
Find full textE, Newton James, and United States. National Aeronautics and Space Administration., eds. Measurement of local convective heat transfer coefficients from a smooth and roughened NACA-0012 airfoil: Flight test data. National Aeronautics and Space Administration, 1988.
Find full textE, Newton James, and United States. National Aeronautics and Space Administration., eds. Measurement of local convective heat transfer coefficients from a smooth and roughened NACA-0012 airfoil: Flight test data. National Aeronautics and Space Administration, 1988.
Find full textPoinsatte, Philip E. Heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis Icing Research Tunnel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textS, Hill Acquilla, and Langley Research Center, eds. High Reynolds number transonic tests of an NACA 0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel. National Aeronautics and Space Administration, Langley Research Center, 1988.
Find full textPoinsatte, Philip E. Convective heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis icing research tunnel. NASA, 1990.
Find full textPoinsatte, Philip E. Convective heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis icing research tunnel. NASA, 1990.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textDyken, Robert D. Van. Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000. Naval Postgraduate School, 1997.
Find full textJohn, Hansman Robert, and United States. National Aeronautics and Space Administration, eds. An experimental low Reynolds number comparison of a Wortmann FX67-K170 airfoil, a NACA 0012 airfoil, and a NACA 64-210 airfoil in simulated heavy rain: Final report to the NASA Langley Research Center on work accomplished under research grant NAG-1-568. National Aeronautics and Space Administration, 1987.
Find full textR, Mohler Stanley, and United States. National Aeronautics and Space Administration., eds. Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet. National Aeronautics and Space Administration, 1995.
Find full textNational Aeronautics and Space Administration (NASA) Staff. NACA 0015 Wing Pressure and Trailing Vortex Measurements. Independently Published, 2018.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Pressure Distributions from Subsonic Tests of a NACA 0012 Semispan Wing Model. Independently Published, 2018.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Effect of Full-Chord Porosity on Aerodynamic Characteristics of the NACA 0012 Airfoil. Independently Published, 2018.
Find full textNeef, Hendrick. Grundlagen Elektrotechnik: Theorieteil EffT Nach DGUV Grundsatz 303-001. Independently Published, 2019.
Find full textPosso Pacheco, Richar Jacobo, Bertha Susana Paz Viteri, Lexy Lázaro Figueredo Frutos, et al. Necesidades educativas especiales en el contexto de la educación física. Universidad Pedagógica Experimental Libertador, Instituto Pedagógico de Barquisimeto "Luis Beltrán Prieto Figueroa", 2022. http://dx.doi.org/10.46498/upelipb.lib.0015.
Full textWall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Find full textPredicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textNeef, Hendrick. Schutz Gegen Elektrischen Schlag: Theorieteil EffT Nach DGUV Grundsatz 303-001. Independently Published, 2019.
Find full textNeef, Hendrick. Grundlagen Elektrotechnik - Band 1: EuP und EffT Nach DGUV Grundsatz 303-001. Independently Published, 2019.
Find full textNeef, Hendrick. Gefahren und Auswirkungen des Elektrischen Stroms: Theorieteil EffT Nach DGUV Grundsatz 303-001. Independently Published, 2018.
Find full textA flow visualization study of the leading edge separation bubble on a NACA 0012 airfoil with simulated glaze ice. National Aeronautics and Space Administration, 1988.
Find full textPressure distributions from high Reynolds number transonic tests of an NACA 0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel. National Aeronautics and Space Administration, Langley Research Center, 1988.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Effects of Independent Variation of Mach and Reynolds Numbers on the Low-Speed Aerodynamic Characteristics of the NACA 0012 Airfoil Section. Independently Published, 2018.
Find full textVossberg, Andreas. FTIR- und Polarisations-FTIR-ATR-spektroskopische Untersuchungen zur Adsorption von Wasserstoff und Deuterium an reinen und NaCl-bedampften NaCl(001)-Einkristall-Oberflächen. 1998.
Find full textCowles, Lisa J. High Reynolds number, low Mach number, steady flow field calculations over a NACA 0012 airfoil using Navier-Stokes and Interactive Boundary Layer theory. 1987.
Find full textExperimental and Computational Analysis of Separation Bubble Behavior for Compressible Steady and Oscillatory Flows Over a NACA 0012 Airfoil (M=0.3, Re=540,000). Storming Media, 1997.
Find full textCollection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet. National Aeronautics and Space Administration, 1995.
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