Books on the topic 'Delta Wing Aerodynamics'

Craig, 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.

Doggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.

Doggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.

Doggett, Robert V. Some low-speed flutter characteristics of simple low-aspect-ration delta wing models. National Aeronautics and Space Administration, Langley Research Center, 1989.

Erickson, Gary E. Effects of forebody strakes and Mach number on overall aerodynamic characteristics on configuration with 55ʻ́ cropped delta wing. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Mourtos, Nikos J. The aerodynamics of delta wings of elliptical cross-section with separated flow. Stanford University, Dept. of Aeronautics and Astronautics, 1985.

Erickson, 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.

Beukenberg, M. Aerodynamische Untersuchungen an Doppeldeltaflügeln bei unsymmetrischer Strömung =: Aerodynamic investigations on double-delta-wings in unsymmetrical flow. Dokumentationszentrum der Bundeswehr, 1987.

McMillin, S. Naomi. Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings: A correlation with experiment. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

McMillin, S. Naomi. Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings: A correlation with experiment. Langley Research Center, 1990.

Menzies, Margaret Anne. Unsteady, transonic flow around delta wings undergoing coupled and natural modes response: A multidisciplinary problem. Old Dominion University, 1996.

United States. National Transportation Safety Board. Aircraft accident report: Delta Air Lines, Inc., Lockheed L-1011-385-1, N726DA, Dallas/Fort Worth-International Airport, Texas, August 2, 1985. The Board, 1986.

Study of lee-side flows over conically cambered delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

B, 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.

Pressure measurements on a thick cambered and twisted 58ʻ́. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Leading edge vortex dynamics on a pitching delta wing: A thesis. Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, 1990.

A, 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.

Shigeru, 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.

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.

M, 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.

M, 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.

T, 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.

D, Hoffler Keith, and Langley Research Center, eds. A low speed wind tunnel study of vortex interaction control techniques on a chine-forebody/delta-wing configuration. National Aeronautics and Space Administration, Langley Research Center, 1992.

Center, 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.

A, Tavella D., and Joint Institute for Aeronautics and Acoustics, eds. Analytical observations on the aerodynamics of a delta wing with leading edge flaps. Stanford University, Dept. of Aeronautics and Astronautics, 1986.

F, 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.

E, Byrd James, Wesselmann Gary F, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

United 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.

E, Reubush David, Haddad Raymond C, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

E, Reubush David, Haddad Raymond C, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers. National Aeronautics and Space Administration, Langley Research Center, 1992.

K, Bhat M., and Langley Research Center, eds. High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers. National Aeronautics and Space Administration, Langley Research Center, 1992.

High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers. National Aeronautics and Space Administration, Langley Research Center, 1992.

K, Bhat M., and Langley Research Center, eds. Subsonic investigations of vortex interaction control for enhanced high-alpha aerodynamics of a chine forebody/delta wing configuration. National Aeronautics and Space Administration, Langley Research Center, 1992.

Supersonic aerodynamics of delta wings. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

L, Soistmann D., Bennett Robert M. 1945-, and Langley Research Center, eds. Flutter analysis of highly swept delta wings by conventional methods. National Aeronautics and Space Administration, Langley Research Center, 1989.

Oktay, Baysal, and United States. National Aeronautics and Space Administration., eds. Three-dimensional aerodynamic shape optimization of supersonic delta wings: [abstract]. American Institute of Aeronautics and Astornautics, 1994.

Oktay, Baysal, and United States. National Aeronautics and Space Administration., eds. Three-dimensional aerodynamic shape optimization of supersonic delta wings: [abstract]. American Institute of Aeronautics and Astornautics, 1994.

Oktay, Baysal, and United States. National Aeronautics and Space Administration., eds. Three-dimensional aerodynamic shape optimization of supersonic delta wings: [abstract]. American Institute of Aeronautics and Astornautics, 1994.

F, Covell Peter, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

M, Ware George, MacConochie Ian O, and Langley Research Center, eds. Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle. National Aeronautics and Space Administration, Langley Research Center, 1996.

Center, Ames Research, ed. Theoretical studies on flapped delta wings. National Aeronautics and Space Administration, Ames Research Center, 1988.

Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis: Abstract. National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis: Abstract. National Aeronautics and Space Administration, 1995.