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LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A 17-PERCENT-THICK AIRFOIL SECTION DESIGNED FOR GENERAL AVIATION APPLICATIONS

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BookPublisher: Nasa, Washington, D.C. 1973Description: 69.DDC classification: NASA | TN D-7428 -

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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-7428 - (Browse shelf)	Not for loan		TR7651

Total holds: 0

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Previous	NASA TN D-7424 APPLICATION OF BOUNDARY INTEGRAL METHOD TO ELASTIC ANALYSIS OF V-NOTCHED BEAMS	NASA TN D-7426 - THERMAL-EXPANSION METHOD FOR LINING TANTALUM ALLOY TURBING WITH TUNGSTEN	NASA TN D-7427 - HYPERSONIC AERODYNAMIC CHARACTERISTICS OF A FAMILY OF POWER-LAW, WING-BODY CONFIGURATIONS	NASA TN D-7428 - LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A 17-PERCENT-THICK AIRFOIL SECTION DESIGNED FOR GENERAL AVIATION APPLICATIONS	NASA TN D-7430 - HEAT-TRANSFER AND PRESSURE DISTRIBUTIONS FOR LAMINAR SEPARATED FLOWS DOWNSTREAM OF REARWARD-FACING STEPS WITH AND WITHOUT MASS SUCTION	NASA TN D-7432 - OPTIMIZATION OF WAVE CANCELLATION IN THEVARIABLE POROSITY TRANSONIC WIND TUNNEL FLOWS	NASA TN D-7433 - CONTIMINATION ASSESSMENT AND CONTROL IN SCIENTIFIC SATELLITES	Next

Bound With Nasa Tn D-7425-30

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