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NASA Technical Note D-7635; Differential Analysis for the Turbulent Boundary Layer on a Compressor Blade Element (Including Boundary-Layer seperaton)
Published by NASA, Lewis Research Center, 1974
£ 15.34
Convert currency£ 39.46 shipping from U.S.A. to United KingdomQuantity: 1 available
Add to basketStapled Printed Wraps. Condition: VG-. 28pp. Illustrated with physics formulae, charts, graphs, drawings, etc. Experimental aviation, rocketry, mechanics and theory, etc. Size: 4to - over 9¾" - 12" tall.
