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ON THE USE OF THICK-AIRFOIL THEORY TO DESIGN AIRFOIL FAMILIES IN WHICH THICKNESS AND LIFT ARE VARIED INDEPENDENTLY

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BookPublisher: Nasa, Washington, D.C. 1974Description: 13.DDC classification: NASA | TN D-7579 -

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-7579 - (Browse shelf)	Not for loan		TR9990

Total holds: 0

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Previous	NASA TN D-7576 - FLIGHT TEST OF A PRESSURIZATION SYSTEM USED TO MEASURE MINOR ATMOSPHERIC CONSTITUENTS FORM AN AIRCRAFT	NASA TN D-7577 - Effect of surface topography on structural growth of thick sputtered films	NASA TN D-7578 - TEXTURING AND RESIDUAL STRESS IN METALS AS A RESULT OF SLIDING	NASA TN D-7579 - ON THE USE OF THICK-AIRFOIL THEORY TO DESIGN AIRFOIL FAMILIES IN WHICH THICKNESS AND LIFT ARE VARIED INDEPENDENTLY	NASA TN D-758 - HEAT-TRANSFER TESTS OF 20-MILLIMETER PROJECTILES AT A MACH NUMBER OF 5 WITH AN ANALYSIS BY UNSTEADY SCALING LAWS TO PREDICT COMPONENT TEMPERATURE RISES AFTER FIRING FOR VARIOUS FREE -FLIGHT CONDITIONS	NASA TN D-7580 - ALGORITHM FOR A GENERAL CLASS OF ROUTINE PROBLEMS DERIVED FROM HUYGENS' PRINCIPLE	NASA TN D-7582 - SYSTEM FOR SPACECRAFT ATTITUDE CONTROL AND ENERGY STORAGE	Next

Bound With Nasa Tn D-7571-80

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