EFFECT OF TRANSVERSE SURFACE CURVATURE IN THE CHARACTERISTICS OF A NONISOTHERMAL AXIALLY SYMMETRICAL TURBULENT BOUNDARY LAYER OF COMPRESSIBLE GAS,
Abstract
Contents: Initial system of equations, boundary conditions; Temperature distribution in boundary layer; Velocity profile and resistance law; Integration of pulse equation; Determination of boundary layer characteristics; Effect of transverse surface curvature on the friction resistance coefficient at various Reynolds, Mach numbers and temperature factor; Comparison of calculation and experimentation data; Derivation of formulas for r* and s.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 21, 1967
- Accession Number
- AD0661906
Entities
People
- A. S. Ginevskii
- E. E. Solodkin
Organizations
- National Air and Space Intelligence Center