Accession Number:

AD0671120

Title:

FLUID AND GAS DYNAMICS (SELECTED ARTICLES),

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Kapustyanskii,S. M.
• Krivtsova,N. V.
• Yakovenko,V. V.

Report Date:

1967-09-22

Pagination or Media Count:

38.0

Abstract:

Contents One-parameter solution of equations of laminar boundary layer in gas flow of large speeds with the Prandtl not equal to unity Laminar boundary layer in equilibrium-dissociated gas Total aerodynamic characteristics of a thick wing in unsteady motion.

Descriptors:

• (*LAMINAR BOUNDARY LAYER
• AERODYNAMIC CHARACTERISTICS)
• (*WINGS
• AERODYNAMIC CHARACTERISTICS)
• OSCILLATION
• EQUATIONS OF MOTION
• PRANDTL NUMBER
• DISSOCIATION
• NUMERICAL ANALYSIS
• THICKNESS
• USSR

Subject Categories:

• Aerodynamics
• Aircraft
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE