Accession Number:

AD0625095

Title:

MEASUREMENT OF THE HEAT TRANSFER TO A TWO-DIMENSIONAL HYPERSONIC INLET WITH VARIABLE GEOMETRY.

Descriptive Note:

Technical rept.,

Corporate Author:

CINCINNATI UNIV OHIO DEPT OF AEROSPACE ENGINEERING

Personal Author(s):

• Tabakoff,Widen
• mcDonel,James D.

Report Date:

1965-11-01

Pagination or Media Count:

41.0

Abstract:

The report describes the experimental measurement of aerodynamic heat transfer to a two-dimensional variable geometry hypersonic inlet model. The program was conducted in a twenty-inch hypersonic tunnel. Testing was at a nominal free stream Mach number of 14 and free stream Reynolds numbers of 721,000 and 631,000 per foot. The experimental results are compared to an approximate theoretical solution for laminar boundary layer flow over a flat plate. Author

Descriptors:

• *HEAT TRANSFER
• *DUCT INLETS
• HYPERSONIC FLOW
• TWO DIMENSIONAL
• LAMINAR BOUNDARY LAYER
• GEOMETRIC FORMS
• MEASUREMENT

Subject Categories:

• Fluid Mechanics
• Thermodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE