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INVESTIGATION AT TRANSONIC SPEEDS OF THE LOADING OVER A 45 DEGREE SWEPTBACK WING HAVING AN ASPECT RATIO OF 3, A TAPER RATIO OF 0.2, AND NACA 65A004 AIRFOIL SECTIONS

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BookPublisher: Nasa, Washington, D.C. 1961Description: 93.DDC classification: NASA | TN D-712

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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-712 (Browse shelf)	Not for loan		TR12613

Total holds: 0

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Previous	NASA TN D-7117 EFFECT OF AUTOCLAVE HEAT TREATMENTS ON THE MECHANICAL PROPERTIES OF THE PREALLOYED POWDER COBALT-BASE ALLOY HS-31	NASA TN D-7118 EMISSION OF SOUND FROM TURBULENCE CONVECTED BY A PARALLEL FLOW IN THE PRESENCE OF SOLID BOUNDARIES	NASA TN D-7119 ELASTOSTATIC STRESS ANALYSIS OF ORTHOTROPIC RECTANGULAR CENTER-CRACKED PLATES	NASA TN D-712 INVESTIGATION AT TRANSONIC SPEEDS OF THE LOADING OVER A 45 DEGREE SWEPTBACK WING HAVING AN ASPECT RATIO OF 3, A TAPER RATIO OF 0.2, AND NACA 65A004 AIRFOIL SECTIONS	NASA TN D-7121 ELASTOHYDRODYNAMIC ANALYSIS USING A POWER LAW PRESSURE-VISCOSITY RELATION.	NASA TN D-7122 ELECTRON PARAMAGNETIC RESONANCE STUDIES OF A VISCOUS NEMATIC LIQUID CRYSTAL-EVIDENCE COUNTER TO A SECOND-ORDER PHASE CHANGE.	NASA TN D-7123 DISSOCIATION ENERGIES OF SOME HIGH TEMPERATURE MOLICULES CONTAINING ALUMINUM.	Next

Bound With Nasa Tn D-701-11, 713-20

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