Accession Number:

ADA067105

Title:

Tip Effect of Supersonic Flow Past Dihedral Angle,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Vorob'yev,N. F.

Report Date:

1978-06-22

Pagination or Media Count:

13.0

Abstract:

Descriptors:

• *SUPERSONIC FLOW
• *WING TIPS
• *DIHEDRAL ANGLE
• USSR
• APPROXIMATION(MATHEMATICS)
• TRANSLATIONS
• INTEGRAL EQUATIONS

Subject Categories:

• Aircraft
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE