Books on the topic 'Delta wing'
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Tavella, Domingo A. An analysis of conical augmentor/delta wing integration. Stanford University, Department of Aeronautics and Astronautics, 1987.
Find full textWood, Richard M. Study of lee-side flows over conically cambered delta wings at supersonic speeds. Langley Research Center, 1987.
Find full textB, Watson Carolyn, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Study of lee-side flows over conically cambered delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.
Find full textHu, B. K. The performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wing. Cranfield Institute of Technology, College of Aeronautics, 1990.
Find full textLeonard, Roberts, and United States. National Aeronautics and Space Administration., eds. Controlled vortical flow on delta wings through unsteady leading edge blowing. Stanford University, Dept. of Aeronautics and Astronautics, Joint Institute for Aeronautics and Acoustics, 1990.
Find full textKjelgaard, Scott O. Detailed flow-field measurements over a 75⁰ swept delta wing. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textKjelgaard, Scott O. Detailed flow-field measurements over a 75⁰ swept delta wing. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textLee, Chyang S. Experimental studies of a delta wing with leading edge flaps. Joint Institute for Aeronautics and Acoustics, 1987.
Find full textTiwari, Surendra N. Numerical solutions of Navier-Stokes equations for a Butler wing. Dept. of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University, 1985.
Find full textA, Tavella D., Roberts Leonard, and United States. National Aeronautics and Space Administration., eds. Numerical study of delta wing leading edge blowing. Joint Institute for Aeronautics and Acoustics, 1988.
Find full textLee, Elizabeth M. Conical Euler solution for a highly-swept delta wing undergoing wing-rock motion. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textYip, Long P. Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform. Langley Research Center, 1990.
Find full textYip, Long P. Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform. Langley Research Center, 1990.
Find full textCenter, Langley Research, ed. Transonic Navier-Stokes calculations about a 65⁰ delta wing. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textCenter, Langley Research, ed. Transonic Navier-Stokes calculations about a 65⁰ delta wing. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textCenter, Langley Research, ed. Transonic Navier-Stokes calculations about a 65⁰ delta wing. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textLondenberg, W. Kelly. Transonic Navier-Stokes calculations about a 65 degree Delta wing. Langley Research Center, 1994.
Find full textKunyi, Cheng, ed. Active flutter suppression on a delta wing model structure. DFVLR, 1986.
Find full textChu, Julio. Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds. Langley Research Center, 1987.
Find full textNarayan, Krishnaswami Yegna. Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data. DFVLR, 1988.
Find full textWood, Richard M. Study of lee-side flows over conically cambered delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.
Find full textOld Dominion University. Research Foundation. and United States. National Aeronautics and Space Administration., eds. Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications: Final report for the period December 1, 1995 through Novemeber 30, 1996. Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University, 1997.
Find full textOld Dominion University. Research Foundation. and United States. National Aeronautics and Space Administration., eds. Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications: Final report for the period December 1, 1995 through Novemeber 30, 1996. Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University, 1997.
Find full textAshill, P. R. Control of leading-edge separation on a cambered delta wing. Defence Research Agency, 1993.
Find full textBerglind, Torsten. The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack. Aeronautical Research Institute of Sweden, 1988.
Find full textM, Wood Richard, Miller David S, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full textM, Wood Richard, Miller David S, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Find full textCovell, Peter F. Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds. Langley Research Center, 1987.
Find full textCraig, Ken. Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings. Stanford University, Dept. of Aeronautics and Astronautics, 1991.
Find full textCraig, Ken. Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings. Stanford University, Dept. of Aeronautics and Astronautics, 1991.
Find full textErickson, Gary E. Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing. Langley Research Center, 1992.
Find full textRinoie, Kenichi. Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing. National Aerospace Laboratory, 1992.
Find full textH, Johari, and United States. National Aeronautics and Space Administration., eds. Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching. Mechanical Engineering Dept., Worcester Polytechnic Institute, 1995.
Find full textSeshadri, S. N. Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis. DFVLR, 1989.
Find full textV, Doggett Robert, and Langley Research Center, eds. Experimental transonic flutter characteristics of two 72 ̊-sweep delta-wing models. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textKjelgaard, Scott O. Detailed flow-field measurements over a 75 degree swept delta wing. Langley Research Center, 1990.
Find full textT, Batina John, and Langley Research Center, eds. Conical Euler simulation and active suppression of delta wing rocking motion. National Aeronautics and Space Administration, Langley Research Center, 1990.
Find full textCenter, Ames Research, ed. An aerodynamic model for one and two degree of freedom wing rock of slender delta wings. National Aeronautics and Space Administration, Ames Research Center, 1993.
Find full textE, Walker Charlotte, and Langley Research Center, eds. Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textUnited States. National Aeronautics and Space Administration., ed. The Delta monster: An RPV designed to investigate the aerodynamics of a delta wing platform : final design proposal. Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, 1989.
Find full textO, Kandil, and United States. National Aeronautics and Space Administration., eds. Natural rolling responses of a delta wing in transonic and subsonic flows. American Institute of Aeronautics and Aeronautics, 1996.
Find full textF, Sheta Essam, Massey Steven James, and United States. National Aeronautics and Space Administration., eds. Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow. National Aeronautics and Space Administration, 1997.
Find full textShigeru, Obayashi, and Ames Research Center, eds. A streamwise upwind algorithm applied to vortical flow over a delta wing. National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textThompson, Scott A. Surface pressure distributions on a delta wing undergoing large amplitude pitching oscillations. Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, 1990.
Find full textW, 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. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textDoggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textDoggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textDoggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textUnited States. National Aeronautics and Space Administration., ed. Effective control of computationally simulated wing rock in subsonic flow. National Aeronautics and Space Administration, 1997.
Find full textUnited States. National Aeronautics and Space Administration., ed. Lift augmentation on a delta wing via leading edge fences and the Gurney flap. National Aeronautics and Space Administration, 1992.
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