Accession Number:

AD0257278

Title:

EXPERIMENTAL DETERMINATION OF THE RECOVERY FACTOR AND ANALYTICAL SOLUTION OF THE CONICAL FLOW FIELD FOR A 20 DEGREE INCLUDED ANGLE CONE AT MACH NUMBERS OF 4.6 AND 6.0 AND STAGNATION TEMPERATURES TO 2600 DEGREES R

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C

Personal Author(s):

Report Date:

1961-06-01

Pagination or Media Count:

1.0

Abstract:

The Reynolds number range of the tests conductedAT THE HIGH TEMPERATURES FELL IN THE SLIP-FLOW REGIME. The results indicated, generally, that the recovery factor can be predicted satisfactorily using the square root of the Prandtl number. The recovery data also indicated two definite trends one of decreasing recovery factor with decreasing pressure, and one of decreasing recovery factor with increasing temperature. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE