Accession Number:

AD0618570

Title:

TRANSIENT FLOW FIELD ANALYSIS OF A PLANE BLAST WAVE INTERCEPTING A STATIONARY CONE AT ZERO ANGLE OF ATTACK.

Descriptive Note:

Doctoral thesis,

Corporate Author:

OKLAHOMA STATE UNIV STILLWATER

Personal Author(s):

Report Date:

1965-05-01

Pagination or Media Count:

194.0

Abstract:

A method for the transient analysis for the stationary cone was developed. Extensions of several methods were utilized and made compatible with existing flow conditions to provide a continuous flow solution. Whithams approximate solution was used to obtain the shock diffraction pattern past the forebody. The results of the blast-base interaction solution was used to mate the blast passage with the formation of the separated flow region behind the body. It is shown that the steady-state base flow studies of Zumwalt and Tang provided the method used to accomplish this. The use of Zumwalts conical wake analysis introduced a satisfactory physical model for the jet mixing region which occurs as a result of flow separation.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE