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DISTRIBUTION OF HEAT TRANSFER ON A 10(DEGREE) CONE AT ANGLES OF ATTACK FROM 0(DEGREE) TO 15(DEGREE) FOR MACH NOS.OF 2.49 TO4.65 & A SOLUTION TO THE HEATTRANSFER EQU. THAT PERMITS COMPLETE MACHINE CAL.

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BookPublisher: Nasa, Washington, D.C. 1959Description: 45.DDC classification: NASA | MEMO 6-4-59L -

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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 6-4-59L - (Browse shelf)	Not for loan		TR7871

Total holds: 0

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Previous	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	NASA MEMO 6-29-59L - THREE-DIMENSIONAL LUNAR MISSION STUDIES	NASA MEMO 6-4-59L - DISTRIBUTION OF HEAT TRANSFER ON A 10(DEGREE) CONE AT ANGLES OF ATTACK FROM 0(DEGREE) TO 15(DEGREE) FOR MACH NOS.OF 2.49 TO4.65 & A SOLUTION TO THE HEATTRANSFER EQU. THAT PERMITS COMPLETE MACHINE CAL.	NASA MEMO 6-8-59L - AERODYNAMIC CHARACTERISTICS OF THE X-15/B-52 COMBINATION	NASA MEMO 6-9-59A - TRANSONIC AERODYNAMIC CHARACTERISTICS OF A LATERAL CONTROL EMPLOYING ROTATABLE AIRFOILS MOUNTED VERTICALLY AT THE WING TIPS OF A 45(DEGREE) SWEPTBACK WING, FUSELAGE, AND TAIL COMBINATION	NASA MEMO-12-5-58L - HEATING AND IMPACT TESTS ON INSULATED AND UNINSULATED BALLISTIC-MISSILE FUSE MECHANISMS SUBJECTED TO SIMULATED REENTRY AERODYNAMIC HEATING	Next

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

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