HEAT TRANSFER TO AN INCOMPRESSIBLE TURBULENT BOUNDARY LAYER AND ESTIMATION OF HEAT-TRANSFER COEFFICIENTS AT SUPERSONIC NOZZLE THROATS
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A collection of quarterly reports consisting of the installation and layout design of the air collector system for commercial applications, completion of the preliminary design review, detailed design efforts, and preparation of the verification test plan are given. Performance specifications and performance testing of a prototype model of a two manifold, 144 tube air collector array is presented.
For abstract, see N78-25537.
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