Effects of external influences in subsonic delta wing vortices

Author:

WASHBURN ANTHONY1

Affiliation:

1. Vigyan, Inc., Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. lummel,D: "On the Vortex Formation Overa Slender Wing at Large Angles of Incidence" in High Angle of Attack Aerodynamics,AGARDCP-247,1979. 2emaire,D. A. "SomeObservations of theLow-Speed Flow Over a Sharp-Edged Delta Wing of Unit Aspect Ratio",AeronauticalResearchLaboratoriesAero.Report 126,Jan. 1965.

2. 3eckham,D. H. and Atkinson, S. A. "Preliminary Resultsof Low SpeedTunnelTests on a GothicWing of AspectRatio 1.0",A. R. C.CP-508,April 1957. 4eckham,D. H. "Low-SpeedWind Tunnel Tests on a Seriesof UncamberedSlenderPointedWings with Sharp Edges",A. R. C. R. & M.No. 3186,December 1958.

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