Accession Number:

ADA067192

Title:

The Study of Supersonic Flow Around Delta Wings with Forced Antisymmetry Taking Into Consideration the Falling off of Flow at the Leading Edges,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Staicu,St.

Report Date:

1978-07-06

Pagination or Media Count:

34.0

Abstract:

Descriptors:

• *SUPERSONIC FLOW
• *DELTA WINGS
• AERODYNAMIC CHARACTERISTICS
• TRANSLATIONS
• LEADING EDGES
• FLOW SEPARATION
• PRESSURE DISTRIBUTION
• RUMANIA
• THIN WINGS

Subject Categories:

• Aircraft
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE