Accession Number:

AD0453217

Title:

BOUNDARY-LAYER, PRESSURE, AND TEMPERATURE DISTRIBUTION STUDIES ON SEVERAL ISENTROPIC COMPRESSION SURFACES AT MACH NUMBERS FROM 4 TO 8

Descriptive Note:

Technical documentary rept.

Corporate Author:

ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN

Personal Author(s):

Report Date:

1964-12-01

Pagination or Media Count:

44.0

Abstract:

Boundary-layer, pressure, and temperature measurements were obtained on the generating cylinder and isentropic compression surface of several axisymmetric hypersonic inlet configurations at supersonic and hypersonic Mach numbers. Boundary-layer surveys were performed at selected stations on uncooled Mach 5, 6, and 10 inlets and a cooled Mach 8 inlet. Model surface temperatures and pressures were obtained at several Mach numbers on all configurations. Steady-state heat transfer data were obtained on the Mach 8 inlet at several model wall temperatures. Selected results from the tests are presented.

Subject Categories:

  • Thermodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE