Accession Number:

AD0091844

Title:

INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE EFFECT OF HORIZONTAL-TAIL LOCATION ON LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS OF A COMPLETE MODEL HAVING A SWEPTBACK WING IN A HIGH LOCATION

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

Report Date:

1956-04-18

Pagination or Media Count:

50.0

Abstract:

Subject Categories:

  • Aircraft
  • Theoretical Mathematics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE