Accession Number:

AD0005949

Title:

AN INVESTIGATION AT TRANSONIC SPEEDS OF THE EFFECTS OF FENCES, DROOPED NOSE, AND VORTEX GENERATORS ON THE AERODYNAMIC CHARACTERISTICS OF A WING-FUSELAGE COMBINATION HAVING A 6-PERCENT-THICK, 45 DEG SWEPTBACK WING

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

Report Date:

1953-03-31

Pagination or Media Count:

33.0

Abstract:

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE