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EFFECT OF AFTERBODY-EJECTOR CONFIGURATIONS ON THE PERFORMANCE AT TRANSONIC SPEEDS OF A PYLON-SUPPORTED NACELLE MODEL HAVING A HOT-JET EXHAUST

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BookPublisher: Nasa, Washington, D.C. 1959Description: 53.DDC classification: NASA | MEMO 1-4-59L -

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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 1-4-59L - (Browse shelf)	Not for loan		TR7660

Total holds: 0

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Previous	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	NASA MEMO 1-5-59L - EFFECT OF BEAM LOADING ON WATER IMPACT LOADS AND MOTIONS	NASA MEMO 1-6-59L - INVESTIGATION OF SPHERICAL-WAVE-INITIATED FLOW FIELDS AROUND BODIES	NASA MEMO 1-7-59L - WIND-TUNNEEL INVESTIGATION OF ROTOR BEHAVIOR UNDER EXTREME OPERATING CONDITIONS WITH A DESCRIPTION OF BLADE OSCILLATIONS ATTRIBUTED TO PITCH-LAG COUPLING	Next

Bound With Nasa Memo 1-2-59l-1-10-59l

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