Accession Number:

AD0005479

Title:

ON THE EFFECT OF THICKNESS ON THE DAMPING IN ROLL OF AIRFOILS AT SUPERSONIC SPEEDS

Descriptive Note:

Corporate Author:

ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD

Personal Author(s):

Report Date:

1953-01-01

Pagination or Media Count:

59.0

Abstract:

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE