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EFFECTS OF CROSS-SECTIONAL SHAPE, SOLIDITY, AND DISTRIBUTION OF HEAT-TRANSFER COEFFICIENT ON THE TORISIONAL STIFFNESS OF THIN WINGS SUBJECTED TO AERODYNAMIC HEATING

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BookPublisher: Nasa, Washington, D.C. 1959Description: 31.DDC classification: NASA | MEMO 1-30-59L

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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 MEMO 1-30-59L (Browse shelf)	Not for loan		TR17742

Total holds: 0

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Previous	NASA MEMO 1-25-59L EFFECT OF CONVEX LONGITUDINAL CURVATURE ON THE PLANING CHARACTERISTICS OF A SURFACE WITHOUT DEAD RISE	NASA MEMO 1-26-59L FLIGHT INVESTIGATION OF THE SURFACE PRESSURE DISTRIBUTION AND FLOW FIELD AROUND AN ELLIPTICAL SPINNER	NASA MEMO 1-29-59A - PILOT OPINION STUDY OF LATERAL CONTROL REQUIREMENTS FOR FIGHTER-TYPE AIRCRAFT	NASA MEMO 1-30-59L EFFECTS OF CROSS-SECTIONAL SHAPE, SOLIDITY, AND DISTRIBUTION OF HEAT-TRANSFER COEFFICIENT ON THE TORISIONAL STIFFNESS OF THIN WINGS SUBJECTED TO AERODYNAMIC HEATING	NASA MEMO 1-31-59L PARASITE-DRAG MEASUREMENTS OF FIVE HELICOPTER ROTOR HUBS	NASA MEMO 1-3-59L - MEASUREMENTS OF LOCAL HEAT TRANSFER AND PRESSURE ON SIX 2-INCH-DIAMETER BLUNT BODIES AT A MACH NUMBER OF 4.95 AND AT REYNOLDS NUMBERS PER FOOT UP TO 81X1,0000000	NASA MEMO 1-4-59L - EFFECT OF AFTERBODY-EJECTOR CONFIGURATIONS ON THE PERFORMANCE AT TRANSONIC SPEEDS OF A PYLON-SUPPORTED NACELLE MODEL HAVING A HOT-JET EXHAUST	Next

Bound With Nasa Memo 1-15-59l-27,31, Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l

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