Accession Number : ADA298303

Title :   Stability Derivatives at Supersonic Speeds of Thin Rectangular Wings with Diagonals Ahead of Tip Mach Lines,

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC

Personal Author(s) : Harmon, Sidney M.

PDF Url : ADA298303

Report Date : 1949

Pagination or Media Count : 20

Abstract : NO ABSTRACT DUE TO ILLEGIBILITY OF REPORT (KAR)

Descriptors :   *AERODYNAMIC STABILITY, *SUPERSONIC CHARACTERISTICS, *THIN WINGS, STEADY STATE, STABILITY, ROLL, CONTRAST, THEORY, LINEARITY, RECTANGULAR BODIES, SUBSONIC CHARACTERISTICS, FLIGHT SPEEDS, WING TIPS.

Subject Categories : Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE