Accession Number:

ADA007204

Title:

Evaluation the Effect of Transiency in the Flutter Analysis of Aircraft with the Wing of the Small Elongation in Incompressible Flow,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Nabyullin,E. N.

Report Date:

1975-01-27

Pagination or Media Count:

18.0

Abstract:

Descriptors:

• *DELTA WINGS
• *INCOMPRESSIBLE FLOW
• *FLUTTER
• MATHEMATICAL MODELS
• USSR
• DEFORMATION
• AERODYNAMIC LOADING
• TRANSLATIONS
• PRESSURE DISTRIBUTION

Subject Categories:

• Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE