Accession Number:

AD0029785

Title:

Experimental Influence Coefficients for the Deflection of the Wing of a Full-Scale, Swept-Wing Bomber

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

Report Date:

1954-04-22

Pagination or Media Count:

29.0

Abstract:

Subject Categories:

  • Bombers
  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE