Accession Number:

AD0649702

Title:

CALCULATION OF THE LOAD DISTRIBUTION, AT SUPERSONIC SPEEDS, ON A SWEPTBACK WING OF ARBITRARY PLANFORM.

Descriptive Note:

Technical rept.,

Corporate Author:

ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (ENGLAND)

Personal Author(s):

Report Date:

1966-11-01

Pagination or Media Count:

57.0

Abstract:

A method for calculating the load distribution on a cambered or uncambered sweptback wing, with subsonic leading edges and supersonic or subsonic trailing edges, is described. Evvards method is used for the part of the wing ahead of the trailing edge disturbances, and a lift cancellation method for the part affected by the wake. The formulae derived are put into forms suitable for calculations on a high-speed digital computer. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE