Accession Number:

ADA007673

Title:

Method of Calculation of Unsteady Aerodynamic Loads on the Thin Wing of the Final Elongation, which Accomplishes Elastic Harmonic Oscillations into Subsonic Flow,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1975-01-29

Pagination or Media Count:

24.0

Abstract:

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE