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AN ANALYSIS OF INCREMENTAL HORIZONTAL-TAIL LOADS MEASURED ON A SWEPT-WING BOMBER AIRPLANE IN SIDESLIP MANUVERS.

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BookPublisher: Nasa, Washington, D.C. 1959Description: 34.DDC classification: NASA | TN D-100

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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-100 (Browse shelf)	Not for loan		TR15741

Total holds: 0

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Previous	NASA TN D - COLD CATHODES FOR SEALED-OFF CO2 LASERS	NASA TN D_2133 - LARGE-SCALE WIND TUNNEL TESTS OF ANAIRPLANE MODEL WITH AN UNSWEPT TILT WING OF ASPEECT RATIO 5.5, AND WITH VARIOUS STALL CONTROL DEVICES	NASA TN D-10 ON SERIES EXPANSIONS IN MAGNETIC REYNOLDS NUMBER	NASA TN D-100 AN ANALYSIS OF INCREMENTAL HORIZONTAL-TAIL LOADS MEASURED ON A SWEPT-WING BOMBER AIRPLANE IN SIDESLIP MANUVERS.	NASA TN D-1000 EXPLORATORY TESTS OF THE EFFECTS OF JET PLUMES ON THE FLOW OVER CONE-CYLINDER-FLARE BODIES	NASA TN D-1022 A STUDY OF THE AERODYNAMIC CHARACTERISTICS OF A FIXED GEOMETRY PARAGLIDER CONFIGURATION AND THREE CANOPIES WITH SIMULATED VARIABLE CANOPY INFLATION AT A MACH NUMBER OF 6.6	NASA TN D-1023 TRANSONIC FLUTTER TEST OF A HIGHLY SWEPT ARROW WING WITH AND WITHOUT SIMULATED TRAILING-EDGE-MOUNTED ENGINE MASSES	Next

Bound With Nasa Tn D-91-99.

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