Books on the topic 'Wings, Triangular'

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.

Breitsamter, Christian. Turbulente Strömungsstrukturen an Flugzeugkonfigurationen mit Vorderkantenwirbeln. Utz, Wissenschaft, 1997.

International Hypersonic Waverider Symposium (1st 1990 College Park, Md.). Proceedings of 1st International Hypersonic Waverider Symposium, October 17-19, 1990, University of Maryland, College Park, Maryland, U.S.A. The University, 1990.

Powell, Kenneth G. Vortical solutions of the conical Euler equations. Vieweg, 1990.

United 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.

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.

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.

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.

T, Batina John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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.

Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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.

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.

Shahrad, Gavali, Holst Terry L, and Ames Research Center, eds. Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices. National Aeronautics and Space Administration, Ames Research Center, 1987.

Sharad, Gavali, Holst Terry L, and Ames Research Center, eds. Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices. National Aeronautics and Space Administration, Ames Research Center, 1987.

Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices. National Aeronautics and Space Administration, Ames Research Center, 1987.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. The natural flow wing-design concept. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. The natural flow wing-design concept. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of a powered-lift landing, tracking flow features using overset grids, and simulation of high lift devices on a fighter-lift-and-control wing. MCAT Institute, 1993.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of a powered-lift landing, tracking flow features using overset grids, and simulation of high lift devices on a fighter-lift-and-control wing. MCAT Institute, 1993.

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.

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.

P, Yip Long, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

N, Tiwari S., and United States. National Aeronautics and Space Administration., eds. Numerical solutions of Navier-Stokes equations for a Butler wing. Old Dominion University Research Foundation, 1987.

N, Tiwari S., and Langley Research Center, eds. Numerical solutions of Navier-Stokes equations for a Butler wing: Progress report for the period ending August 31, 1985. Old Dominion University Research Foundation, 1985.