Accession Number:

AD0684639

Title:

SUPERSONIC FLOW AROUND OF A SPHERE BY A COMBUSTIBLE MIXTURE OF GASES WITH CONSIDERATION OF IGNITION DELAY TIME,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1968-08-23

Pagination or Media Count:

29.0

Abstract:

A numerical resolution is given of the problem of flow around a sphere by a fuel mixture with the simplest model of the structure of the burn zone in which the whole flow after the forward shock consists of two regions of adiabatic flow - the induction region and the region of equilibrium flow of combustion products, divided by the burn front, in which the mixture burns instantly. A solution is given only for the subsonic and transonic regions of flow. Author

Subject Categories:

  • Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE