EFFECT OF TRANSVERSE SURFACE CURVATURE IN THE CHARACTERISTICS OF A NONISOTHERMAL AXIALLY SYMMETRICAL TURBULENT BOUNDARY LAYER OF COMPRESSIBLE GAS,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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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.
- Fluid Mechanics