Accession Number:

AD0644180

Title:

HYPERSONIC FLOW AROUND AXISYMMETRIC BODIES FLYING AT AN ANGLE OF ATTACK,

Descriptive Note:

Corporate Author:

LOCKHEED MISSILES AND SPACE CO SUNNYVALE CALIF

Personal Author(s):

• Minostsev,V. B.

Report Date:

1961-01-01

Pagination or Media Count:

12.0

Abstract:

The report presents the solution of the problem of angle-of-attack flow around axisymmetric bodies by an ideal gas moving at hypersonic velocities. The problem is solved by the method of expanding the desired flow characteristics in a series in the parameter epsilon gamma-1gamma 1, where gamma is the adiabatic coefficient. The solution is obtained in quadratures in a first approximation. Author

Descriptors:

• *HYPERSONIC FLOW
• AXISYMMETRIC FLOW
• ANGLE OF ATTACK
• BOUNDARY LAYER
• DIFFERENTIAL EQUATIONS
• HYPERSONIC FLIGHT
• APPROXIMATION(MATHEMATICS)
• USSR

Subject Categories:

• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE