Accession Number:

ADA409142

Title:

Numerical Investigation of Interaction of Oblique Shock and Detonation Waves in a Steady Supersonic Flow of a Chemical Reactive Gaseous Mixture

Descriptive Note:

Conference paper

Corporate Author:

RUSSIAN ACADEMY OF SCIENCES NOVOSIBIRSK INST OF THEORETICAL AND APPLIED MECHANICS

Personal Author(s):

• Trotsyuk, A. V.
• Kudryavtsev, A. N.
• Ivanov, M. S.

Report Date:

2002-07-01

Pagination or Media Count:

7.0

Abstract:

The main objective of the present work is to study the flow structure with reflection of oblique SW and DW in a steady supersonic flow of a chemically reacting mixture and the transition from regular to Mach reflection.

Descriptors:

• *GAS DYNAMICS
• *NUMERICAL METHODS AND PROCEDURES
• SHOCK WAVES
• REFLECTION
• SUPERSONIC FLOW
• STEADY FLOW
• DETONATION WAVES

Subject Categories:

• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE