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SHOCK WAVES AND DRAG IN THE NUMERICAL CALCULATION OF ISENTROPIC TRANSONIC FLOW.

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BookPublisher: Nasa, Washington, D.C. 1972Description: 41.DDC classification: NASA | TN D-6997

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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-6997 (Browse shelf)	Not for loan		TR12381

Total holds: 0

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Previous	NASA TN D-6994 APPLICATION OF THE LEADING-EDGE-SUCTION ANALOGY TO PREDICTION OF LONGITUDINAL LOAD DISTRIBUTION AND PITCHING MOMENTS FOR SHARP-EDGED DELTA WINGS	NASA TN D-6995 EFFECT OF RESIDUAL STRESSES INDUCED BY PRESTRESSING ON ROLLING-ELEMENT FATIGUE LIFE.	NASA TN D-6996 PREDICTION OF STATIC AERODYNAMIC CHARACTERISTICS FORSPACE-SHUTTLE-LIKE AND OTHER BODIES AT ANGLES OF ATTACK FROM 0 DEGREE TO 180 DEGREE.	NASA TN D-6997 SHOCK WAVES AND DRAG IN THE NUMERICAL CALCULATION OF ISENTROPIC TRANSONIC FLOW.	NASA TN D-6998 A METHOD FOR CALCULATING LAMINAR VISCOUS, COMPRESSIBLE FLOWS WITH SMALL PRESSURE GRADIENTS.	NASA TN D-6999 EFFECT OF NITROGEN ON TENSILE PROPERTIES AND STRUCTURES OF T-111 (TANTALUM-8-PERCENT-TUNGSTEN-2-PERCENT-HAFNIUM) TUBING.	NASA TN D-7 WING-ON AND WING-OFF LONGITUDINAL CHARACTERISTICS OF AN AIRPLANE CONFIGURATION HAVING A THIN UNSWEPT WING OF ASPECT RATIO 3, AS OBTAINED FROM ROCKET-PROPELLED MODELS AT MACH NUMBERS FROM 0.8 TO 1.4	Next

Bound With Nasa Tn D-6990-96, 6998-99

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