Accession Number:

ADA061935

Title:

Studies and Research on Applied Mechanics (Selected Articles).

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1978-08-30

Pagination or Media Count:

69.0

Abstract:

Contents The Supersonic Flow Around Symmetrical Torsioned and Curved Delta Wings, Taking Into Consideration the Separation of Flow at the Leading Edges and The Thin Delta Wing, With Variable Geometry, Optimum for Two Supersonic Cruising Speeds.

Descriptors:

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

Subject Categories:

• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE