Accession Number:

AD0600422

Title:

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

Descriptive Note:

Corporate Author:

ADELPHI UNIV GARDEN CITY NY

Personal Author(s):

Report Date:

1964-05-01

Pagination or Media Count:

49.0

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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE