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TRANSITION OF THE LAMINAR BOUNDARY LAYER ON A DELTA WING WITH 74 DEGREE SWEEP IN FREE FLIGHT AT MACH NUMBERS FROM 2.8 TO 5.3

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BookPublisher: Nasa, Washington, D.C. 1961Description: 42.DDC classification: NASA | TN D-1066

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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-1066 (Browse shelf)	Not for loan		TR15893

Total holds: 0

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Previous	NASA TN D-1062 A DIGITAL SOLAR ASPECT SENSOR	NASA TN D-1063 THE EFFECT OF SOLAR RADIATION PRESSURE ON THE MOTION OF AN ARTIFICAL SATELLITE.	NASA TN D-1065 ON THE ELECTRON DENSITY DISTRIBUTION ABOVE THE F2 PEAK.	NASA TN D-1066 TRANSITION OF THE LAMINAR BOUNDARY LAYER ON A DELTA WING WITH 74 DEGREE SWEEP IN FREE FLIGHT AT MACH NUMBERS FROM 2.8 TO 5.3	NASA TN D-1067 THE EFFECT OF LATERAL- AND LONGITUDINAL-RANGE CONTROL ON ALLOWABLE ENTRY CONDITIONS FOR A PINT RETURN FROM SPACE.	NASA TN D-1068 SATELLITE ATTITUDE CONTROL UTLIZING THE EARTHS MAGNETIC FIELD.	NASA TN D-1069 EFFECTS OF FLIGHT CONDITIONS AT BOOSTER SEPRATION ON PLLAYLOAD WEIGHT IN ORBIT.	Next

Bound With Nasa Tn D-1061-1065,1067-1070.

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