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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

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BookPublisher: Nasa, Washington, D.C. 1960Description: 41.DDC classification: NASA | TN D-7

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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-7 (Browse shelf)	Not for loan		TR15301

Total holds: 0

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Previous	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	NASA TN D-7001 ANNULAR SLIT COLLOID THRUSTER RESEARCH AND DEVELOPMENT	NASA TN D-7002 FORCES DUE TO AIR AND HELIUM TETS IMPINGING NORMAL TO A FLAT PLATE FOR NEAR-VACUUM AND SEA-LEVEL AMBIENT PRESSURES	NASA TN D-7005 ABLATION PERFORMANCE OF GLASSLIKE CARBONS, PYROLYTIC GRAPHITE, AND ARTIFICIAL GRAPHITE IN THE STAGNATION PRESSURE RANGE 0.035 TO 15 ATMOSPHERES	Next

Bound With Nasa Tn D-1-6,9-10 Lack No.8

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