Accession Number:

ADA007178

Title:

Experimental Study of Heat Transfer on Flat Plate During the Interaction of Oblique Shock Wave with Laminar Boundary Layer,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Kondratev,I. A.

Report Date:

1975-01-08

Pagination or Media Count:

21.0

Abstract:

Descriptors:

• *HEAT TRANSFER
• *SUPERSONIC CHARACTERISTICS
• *LAMINAR BOUNDARY LAYER
• USSR
• INTERACTIONS
• SHOCK WAVES
• ANGLE OF ARRIVAL
• MODEL TESTS
• TRANSLATIONS
• HYPERSONIC CHARACTERISTICS
• AERODYNAMIC HEATING
• FLAT PLATE MODELS

Subject Categories:

• Aerodynamics
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE