Accession Number:

AD0092214

Title:

INVESTIGATION AT HIGH SUBSONIC SPEEDS OF SOME EFFECTS OF SIDESLIP ON THE AERODYNAMIC LOADS ON FINNED AND UNFINNED BODIES MOUNTED FROM THE SWEPT-WING OF A WING-FUSELAGE MODEL

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

Report Date:

1956-04-26

Pagination or Media Count:

56.0

Abstract:

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE