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EXPERIMENTAL INVESTIGATION OF THE HEAT-TRANSFER RATE TO A SERIES OF 20(DEGREE) CONES OF VARIOUS SURFACE FINISHES AT A MACH NUMBER OF 4.95

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BookPublisher: Nasa, Washington, D.C. 1959Description: 26.DDC classification: NASA | MEMO 6-10-59L -

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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 6-10-59L - (Browse shelf)	Not for loan		TR7873

Total holds: 0

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Previous	NASA MEMO 5-25-59L INVESTIGATION OF THE STABILITY OF VERY FLAT SPIN AND ANALYSIS OF EFFECTS OF APPLYING VARIOUS MOMENTS UTILIZING THE THREE MOMENT EQUATIONS OF MOTION	NASA MEMO 5-26-59L MODIFIED MATRIX METHOD FOR CALCULATING STEADY-STATE SPAN LODING ON FLEXIBLE WINGS IN SUBSONIC FLIGHT	NASA MEMO 5-28-59L INVESTIGATION ON THE USE OF A FREELY ROTATING ROTOR AT THE COWL FACE OF A SUPERSONIC CONICAL INLET TO REDUCE INLET FLOW DISTORTION	NASA MEMO 6-10-59L - EXPERIMENTAL INVESTIGATION OF THE HEAT-TRANSFER RATE TO A SERIES OF 20(DEGREE) CONES OF VARIOUS SURFACE FINISHES AT A MACH NUMBER OF 4.95	NASA MEMO 6-11-59L - LOW-SPEED INVES. OF THE EFFECTS OF HORIZONTAL-TAIL AREA & WING SWEEP ON THE STATIC LONGITUDINAL STABILITY & CONTROL CHARS. OF AN AIRPLANE CONFIGURATION HAVING TAIL SURFACES OUTBOARD OF THE WING TIPS	NASA MEMO 6-14-59L - DETERMINATION OF STATIC STRENGTH AND CREEP BUCKLING OF UNSTIFFENED CIRCULAR CYLINDERS SUBJECTED TO BENDING AT ELEVATED TEMPERATURES	NASA MEMO 6-2-59L - COMPRESSIVE STRENGTH OF STAINLESS-STEEL SANDWICHES AT ELEVATED TEMPERATURES	Next

Bound With Nasa Memo 6-1-59l-6-29-59l

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