Accession Number : AD0600422

Title :   AN ASYMPTOTIC METHOD FOR DETERMINING THE LIFT DISTRIBUTION OF A SWEPT-BACK WING OF FINITE SPAN

Corporate Author : ADELPHI UNIV GARDEN CITY NY

Personal Author(s) : Thurber,James K.

Report Date : MAY 1964

Pagination or Media Count : 49

Abstract : A description is given of the flow about a flat, swept-back, symmetrically shaped airfoil which is moving with constant velocity V through a perfect ideal fluid filling three dimensional space. (Author)

Descriptors :   (*AIRFOILS, LIFT), (*LIFT, DISTRIBUTION), (*SWEPTBACK WINGS, LIFT), BOUNDARY LAYER, MATHEMATICAL ANALYSIS

Distribution Statement : APPROVED FOR PUBLIC RELEASE