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COMPARISON OF EXPERIMENTAL AND NUMERICAL RESULTS FOR THE FLOW OF A PERFECT GAS ABOUT BLUNT-NOSED BODIES

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BookPublisher: Nasa, Washington, D.C. 1962Description: 40.DDC classification: NASA | TN D-1426

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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-1426 (Browse shelf)	Not for loan		TR14853

Total holds: 0

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Previous	NASA TN D-1423 PREDICTED GAS PROPERTIES IN THE SHOCK LAYER AHEAD OF CAPSULE-TYPE VEHICLES AT ANGLES OF ATTACK	NASA TN D-1424 RADIATIVE HEAT TRANSFER AND ABSORPTION BEHIND A HYPERSONIC NORMAL SHOCK WAVE	NASA TN D-1425 FREE-FLIGHT TESTS OF FIFTH-STAGE SCOUT ENTRY VEHICLE AT MACH NUMBERS OF 5 AND 17	NASA TN D-1426 COMPARISON OF EXPERIMENTAL AND NUMERICAL RESULTS FOR THE FLOW OF A PERFECT GAS ABOUT BLUNT-NOSED BODIES	NASA TN D-1427 ATMOSPHERE ENTRIES WITH SPACECRAFT LIFT-DRAG RATIOS MODULATED TO LIMIT DECELERATIONS	NASA TN D-1428 A 1-FOOT HYPERVELOCITY SHOCK TUNNEL IN WHICH HIGH-ENTHALPY,REAL-GAS AIR FLOWS CAN BE GENERATED WITH FLOW TIMES OF ABOUT 180 MILLISECONDS	NASA TN D-1429 THERMODYNAMIC AND TRANSPORT PROPERTY CORRELATION FORMULAS FOR EQUILIBRIUM AIR FROM 1,000(DEGRE) K TO 15,000(DEGRE ) K	Next

Bound With Nasa Tn D-1421-1425,1427-1430

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