Accession Number:

AD0420810

Title:

Second-Order Theory of Optimum Two-Dimensional Wings in Supersonic Flow Including the Effects of Friction

Descriptive Note:

Corporate Author:

BOEING SCIENTIFIC RESEARCH LABS SEATTLE WASH

Personal Author(s):

Report Date:

1963-08-01

Pagination or Media Count:

30.0

Abstract:

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE