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PREDICTION OF STATIC AERODYNAMIC CHARACTERISTICS FORSPACE-SHUTTLE-LIKE AND OTHER BODIES AT ANGLES OF ATTACK FROM 0 DEGREE TO 180 DEGREE.

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BookPublisher: Nasa, Washington, D.C. 1973Description: 37.DDC classification: NASA | TN D-6996

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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-6996 (Browse shelf)	Not for loan		TR12380

Total holds: 0

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Previous	NASA TN D-6993 SUMMARY OF DIRECTIONAL DIVERGENCE CHARACTERISTICS OF SEVERAL HIGH-PERFORMANCE AIRCRAFT CONFIGURATIONS.	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.	Next

Bound With Nasa Tn D-6990-95, 6997-99

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