Accession Number:

AD0611137

Title:

INVESTIGATION OF THE PROCESS OF ENERGY TRANSFER FROM AN INTERMITTENT JET TO SECONDARY FLUID IN AN EJECTOR-TYPE THRUST AUGMENTER.

Descriptive Note:

Final interim summary rept. for 30 Oct 62-3l Mar 64,

Corporate Author:

HILLER AIRCRAFT CORP PALO ALTO CALIF

Personal Author(s):

Report Date:

1964-03-31

Pagination or Media Count:

99.0

Abstract:

Besides application of high-speed temperature measuring instrumentation, a search was made for a digital computer program that could be adapted to the problem. This resulted in the evaluation of the KO code developed by the U. of Cal. Radiation Laboratory. This code uses a numerical differencing method with injection of a Q-term of artificial viscosity whenever an incipient shock condition develops. The addition of the Q-term in appropriate amounts prevents a discontinuity so that the computer program can then handle the shock condition and determine when and where it will develop as well.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE