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SOME EFFECTS OF NOSE BLUNTNESS AND FINENESS RATIO ON THE STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF BODIES OF REVOLUTION AT SUBSONIC SPEEDS

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BookPublisher: Nasa, Washington, D.C. 1961Description: 65.DDC classification: NASA | TN D-650

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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-650 (Browse shelf)	Not for loan		TR13528

Total holds: 0

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Previous	NASA TN D-647 FATIGUE DAMAGE UNDER VARYING STRESS AMPLITUDES	NASA TN D-648 EXTERNAL-DRAG ESTIMATION FOR SLENDER CONICAL DUCTED BODIES AT HIGH MACH NUMBERS AND ZERO ANGLE OF ATTACK	NASA TN D-649 LOADS INDUCED ON A FLAT-PLATE WING BY AN AIR JET EXHAUSTING PERPENDICULARLY THROUGH THE WING AND NORMAL TO A FREE-STREAM FLOW OF MACH NUMBER 2.0	NASA TN D-650 SOME EFFECTS OF NOSE BLUNTNESS AND FINENESS RATIO ON THE STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF BODIES OF REVOLUTION AT SUBSONIC SPEEDS	NASA TN D-6523 - EXPERIMENTAL INVESTIGATION OF LAMINAR GAS JET DIFFUSION FLAMES IN ZERO GRAVITY	NASA TN D-6529 - THIN -SHOCK-LAYER SOLUTION FOR NONEQUILIBRIUM INVISCID HYPERSONIC FLOWS IN EARTH,MARTIAN,AND VENUSIAN ATMOSPHERES	NASA TN D-6572 THEORICAL BUCKLING LOADS OF BORON/ALUMINUM AND GRAPHITE/RESIN FIBER-COMPOSITE ANISOTROPIB	Next

Bound With Nasa Tn D-641-649

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