Accession Number:

AD0672543

Title:

Inviscid Blunt Body Shock Layers (Two-Dimensional Symmetric and Axisymmetric Flows)

Descriptive Note:

Technical Report

Corporate Author:

POLYTECHNIC INST OF BROOKLYN FARMINGDALE United States

Personal Author(s):

• Moretti,Gino

Report Date:

1968-06-01

Pagination or Media Count:

174.0

Abstract:

The results of a time-dependent computation of blunt body shock layers for two-dimensional symmetric and axisymmetric flows are presented in a systematic form for a range of values of the free stream Mach number and bodies of different shapes and variable bluntness. A brief discussion of the relevant features of the computational technique is given. The results are presented in a graphical form the graphs were produced by the computer.

Descriptors:

• SHOCK WAVES
• TWO DIMENSIONAL FLOW
• AXISYMMETRIC FLOW
• BLUNT BODIES
• STAGNATION POINT
• THERMODYNAMICS
• MACH NUMBER
• EQUATIONS OF MOTION
• FLOW FIELDS
• INVISCID FLOW
• Transonic flow
• Hypersonic flow

Subject Categories:

• Aerodynamics
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE