Abstracted In International Aerospace Abstracts. Reproduced from: Recent Developments In Calculation Methods For Turbulent Boundary Layers With Pressure Gradients and Heat Transfer (Turbulent Boundary Layer Calculation, Considering Compressible and Incompressible Flows With Pressure Gradients and Heat Transfer{Rpara} A67-15908.
Reproduction Note
Microform. New York : American Institute of Aeronautics and Astronautics, Technical Information Service, [19--?]