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LOW-SPEED AERODYNAMIC CHARACTERISTICS OF AN AIRFOIL OPTIMIZED FOR MAXIMUM LIFT COEFFICIENT.

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BookPublisher: Nasa, Washington, D.C. 1972Description: 53.DDC classification: NASA | TN D-7071

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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-7071 (Browse shelf)	Not for loan		TR12198

Total holds: 0

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Previous	NASA TN D-7068 NUMERICAL METHOD FOR THE SOLUTION OF LARGE SYSTEMS OF DIFFERENTIAL EQUATIONS OF THE BOUNDARY-LAYER TYPE	NASA TN D-7069 AERODYNAMIC CHARACTERISTICS OF A SWEPT-WING CRUISE MISSILE AT MACH NUMBERS FROM 0.50 TO 2.86	NASA TN D-707 STRUCTURE AND DESIGN CONSIDERATIONS OF THE VANGUARD SLV-5 MAGNETIC FIELD SATELLITE	NASA TN D-7071 LOW-SPEED AERODYNAMIC CHARACTERISTICS OF AN AIRFOIL OPTIMIZED FOR MAXIMUM LIFT COEFFICIENT.	NASA TN D-7072 EFFECTS OF FUEL NOZZLE DESIGN ON PERFORMANCE OF AN EXPERIMENTAL ANNULAR COMBUSTOR USING NATURAL GAS FUEL.	NASA TN D-7073 FRETTING OF SECONDARY-SEAL-RING CANDIDATE MATERIALS IN AIR AT TEMPERATURES TO 816 DEGREE C.	NASA TN D-7074 SUMMARY OF DESIGN AND BLADE-ELEMENT PERFORMANCE DATA FOR 12 AXIAL-FLOW PUMP ROTOR CONFIGURATIONS.	Next

Bound With Nasa Tn D-7070, 7072-79

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