Accession Number:

AD0627065

Title:

SLENDER-AIRFOIL CAMBERLINES WITH POLYGONAL LIFT DISTRIBUTIONS.

Descriptive Note:

Research rept.,

Corporate Author:

NAVAL ORDNANCE TEST STATION CHINA LAKE CALIF

Personal Author(s):

Report Date:

1966-01-01

Pagination or Media Count:

28.0

Abstract:

Nondimensional equations are developed from slenderairfoil theory to determine the geometry and pressure characteristics of a mean line camber that will enable a thin lifting surface to develop an arbitrary, assigned, polygonally shaped lift distribution in two-dimensional inviscid flow. These equations are verified as being adequate for making design decisions. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE