Books on the topic 'Icing of aerodynamic surfaces'
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Foss, Van Zante Judith, and Lewis Research Center, eds. In-flight aerodynamic measurements of an iced horizontal tailplane. National Aeronautics and Space Administration, Lewis Research Center, 1999.
Find full textFoss, Van Zante Judith, and Lewis Research Center, eds. In-flight aerodynamic measurements of an iced horizontal tailplane. National Aeronautics and Space Administration, Lewis Research Center, 1999.
Find full textFoss, Van Zante Judith, and Lewis Research Center, eds. In-flight aerodynamic measurements of an iced horizontal tailplane. National Aeronautics and Space Administration, Lewis Research Center, 1999.
Find full textCenter, NASA Glenn Research, ed. An evaluation of an analytical simulation of an airplane with tailplane icing by comparision to flight data. National Aeronautics and Space Administration, Glenn Research Center, 2000.
Find full textShaw, Robert J. Predictions if airfoil aerodynamic performance degradation due to icing. National Aeronautics and Space Administration, 1989.
Find full textRatvasky, Thomas P. NASA/FAA Tailplane Icing Program overview. National Aeronautics and Space Administration, Glenn Research Center, 2000.
Find full textFoss, Van Zante Judith, Riley James T, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. NASA/FAA Tailplane Icing Program overview. National Aeronautics and Space Administration, Lewis Research Center, 1999.
Find full textBarger, Raymond L. Semianalytic modeling of aerodynamic shapes. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textAllen, Arrington E., American Institute of Aeronautics and Astronautics., NASA Glenn Research Center, and Aerospace Sciences Meeting & Exhibit (36th : 1998 : Reno, Nev.), eds. Aerodynamic calibration of the NASA Lewis icing research tunnel (1997 tests). National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textCenter, NASA Glenn Research, ed. Ice accretions and icing effects for modern airfoils. National Aeronautics and Space Administration, Glenn Research Center, 2000.
Find full textOlsen, W. Experimental evidence for modifying the current physical model for ice accretion on aircraft surfaces. National Aeronautics and Space Administration, 1986.
Find full textJ, Ranaudo Richard, and United States. National Aeronautics and Space Administration., eds. Determination of longitudinal aerodynamic derivatives using flight data from an icing research aircraft. National Aeronautics and Space Administration, 1989.
Find full textN, Tiwari S., and United States. National Aeronautics and Space Administration., eds. Sensitivity analysis and optimization of aerodynamic configurations with blend surfaces. Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University, 1997.
Find full textFoss, Van Zante Judith, Sim Alex, and NASA Glenn Research Center, eds. NASA/FAA Tailplane Icing Program: Flight test report. National Aeronautics and Space Administration, Glenn Research Center, 2000.
Find full textUeda, Tetsuhiko. Unsteady aerodynamic calculations for general configurations by the doublet-point method. National Aerospace Laboratory, 1991.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aerodynamics of combat aircraft controls and of ground effects. AGARD, 1990.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aerodynamics of combat aircraft controls and of ground effects. AGARD, 1990.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textCenter, Langley Research, ed. Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory. National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textC, Gonsalez Jose, Spera David A, and NASA Glenn Research Center, eds. Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel. National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textCenter, Langley Research, ed. System maintenance manual for MASTER: Modeling of aerodynamic surfaces by three dimensional explicit representation. National Aeronautics and Space Administration, Langley Research Center, 1985.
Find full textUnited States. National Aeronautics and Space Administration., ed. A review of ice accretion data from a model rotor icing test and comparison with theory. National Aeronautics and Space Administration, 1991.
Find full textUnited States. National Aeronautics and Space Administration., ed. Effects of ice accretion on aircraft aerodynamics: Final report : NASA grant NAG3-1681. National Aeronautics and Space Administration, 1998.
Find full textBoyle, Christopher. Inviscid aerodynamic predictions of hypersonic elliptical projectiles: A comparative study of the effects of stabilizing surfaces. Naval Postgraduate School, 2000.
Find full textJ, Chung, and Lewis Research Center, eds. Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wing. National Aeronautics and Space Administration, Lewis Research Center, 1999.
Find full textD, Reich Allen, and United States. National Aeronautics and Space Administration., eds. Tests of the performance of coatings for low ice adhesion. National Aeronautics and Space Administration, 1997.
Find full textCenter, Ames Research, ed. Numerical study of steady and unsteady canard-wing-body aerodynamics. National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textR, Miller Dean, Ide Robert F, and United States. National Aeronautics and Space Administration., eds. A study of large droplet ice accretion in the NASA Lewis IRT at near-freezing conditions; Pt. 2. National Aeronautics and Space Administration, 1997.
Find full textBarret, C. Review of our national heritage of launch vehicles using aerodynamic surfaces and current use of these by other nations. George C. Marshall Space Flight Center, 1996.
Find full textJames P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. Lyndon B. Johnson Space Center, 1997.
Find full textJames P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1997.
Find full textJames P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1997.
Find full textJames P. Smith - undifferentiated. X- 38 vehicle 131 flutter assessment. National Aeronautics and Space Administration, 1997.
Find full textUnited States. National Aeronautics and Space Administration., ed. Non-linear unsteady wing theory. National Aeronautics and Space Administration, 1987.
Find full textUnited States. National Aeronautics and Space Administration., ed. Non-linear unsteady wing theory. National Aeronautics and Space Administration, 1987.
Find full textNissim, E. Effect of control surface mass unbalance on the stability of a closed-loop active control system. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Find full textYip, Long P. Wind-tunnel investigation of a full-scale canard-configuredgeneral aviation airplane. National; Aeronautics and Space Administration Scientific and Technical Information Branch, 1985.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Wind-tunnel investigation of a full-scale canard-configured general aviation airplane. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Wind-tunnel investigation of a full-scale canard-configured general aviation airplane. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textGeorge C. Marshall Space Flight Center., ed. Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept. National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil. Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textUnited States. National Aeronautics and Space Administration., ed. Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil. Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, 1996.
Find full textP, Britcher Colin, Old Dominion University. Research Foundation., and United States. National Aeronautics and Space Administration., eds. Experimental optimization methods for multi-element airfoils: Final report. Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University, 1996.
Find full textG, Steenken W., and Hugh L. Dryden Flight Research Center., eds. Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft. National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.
Find full textAvery, Don E. Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textFacility, Dryden Flight Research, ed. A concept for adaptive performance optimization on commercial transport aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1995.
Find full textIn-flight aerodynamic measurements of an iced horizontal tailplane. National Aeronautics and Space Administration, Lewis Research Center, 1999.
Find full textNumerical investigation of the effects of icing on fixed and rotary wing aircraft: Progress report for the period January 1, 1992-June 30, 1992. National Aeronautics and Space Administration, 1992.
Find full textLewis Icing Research Tunnel test of the aerodynamic effects of aircraft ground deicing/anti-icing fluids. National Aeronautics and Space Administration, 1992.
Find full textSmetana, Frederick O. Flight Vehicle Performance and Aerodynamic Control (Aiaa Education Series). AIAA (American Institute of Aeronautics & Ast, 2001.
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