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):

• Navyullin,E. N.

Report Date:

1975-01-29

Pagination or Media Count:

24.0

Abstract:

Descriptors:

• *AERODYNAMIC LOADING
• *THIN WINGS
• USSR
• AERODYNAMIC FORCES
• TRANSLATIONS
• SUBSONIC FLOW
• FLUTTER

Subject Categories:

• Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE