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Application of Monte Carlo technique for determining maneuvering loads from statistical information on airplane motions [NASA TN D-524]

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BookPublisher: Washington, D.C. NASA 1961Description: various pagings.

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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-5153 (Browse shelf)	Not for loan		TR15669

Total holds: 0

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Previous	NASA TN D-515 USE OF SUBSONIC KERNEL FUNCTION IN AN INFLUENCE-COEFFICIENT METHOD OF AEROELASTIC ANALYSIS AND SOME COMPARISONS WITH EXPERIMENT	NASA TN D-5150 SIMULATION STUDIES FOR PLANNING AN IN-FLIGHT EXPERIMENT TO DEFINE MANUAL GUIDANCE AND CONTROL TECHNIQUES FOR LARGE LAUNCH VEHICLES	NASA TN D-5152 EFFECT OF OXYGEN CONCENTRATION ON THE PERFORMANCE OF SYNTHETIC PARAFFING OILS IN SHORT TERM BEARING TESTS FROM 400 DEGREE TO 500 DEGREE F.	NASA TN D-5153 Application of Monte Carlo technique for determining maneuvering loads from statistical information on airplane motions [NASA TN D-524]	NASA TN D-5154 EFFECTS OF TEMERATURE AND ELECTROLYTE CONCENTRATION ON PERFORMANCE OF A FUEL CELL OF THE BACON TYPE.	NASA TN D-5155 DESIGN AND PERFORMANCE OF TWO INTEGRATED CIRCUITS FOR FLUIDIC-CONTROLLED PNEUMATIC STEPPING-MOTOR SYSTEM.	NASA TN D-5156 EXPERIMENTAL BENDING STRENGTH OF AN ATLAS LV-3C BOOSTER BEYOND COMPRESSIVE SKIN WRINKLING	Next

Bound With NASA TN D-5151-5152,5154-5170.Lack No-5159

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