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FLIGHT INVESTIGATION OF SOME EFFECTS OF A VANE-CONTROLLED GUST-ALLEVIATION SYSTEM ON THE WING AND TAIL LOADS OF A TRANSPORT AIRPLANE

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BookPublisher: Nasa, Washington, D.C. 1961Description: 32.DDC classification: NASA | TN D-643

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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-643 (Browse shelf)	Not for loan		TR13521

Total holds: 0

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Previous	NASA TN D-6388 EQUIVALENT MEASUREMENTS, OBSERVABILITY,AND CALIBRATION ACCURACY LIMITS IN LINEAR ESTIMATION.	NASA TN D-640 AERODYNAMIC CHARACTERISTICS OF A MODEL OF AN INFLATABLE-SPHERE LAUNCHING VEHICLE UNDER SIMULATED CONDITIONS OF MACH NUMBER AND ALTITUDE	NASA TN D-642 EFFECT OF SHOCK IMPINGEMENT ON THE DISTRIBUTION OF HEAT-TRANSFER COEFFICIENTS ON A RIGHT CIRCULAR CYLINDER AT MACH NUMBERS OF 2.65, 3.51, AND 4.44	NASA TN D-643 FLIGHT INVESTIGATION OF SOME EFFECTS OF A VANE-CONTROLLED GUST-ALLEVIATION SYSTEM ON THE WING AND TAIL LOADS OF A TRANSPORT AIRPLANE	NASA TN D-644 A STUDY OF THE OXIDATION OF MATERIALS IN AN ARC -IMAGE FURNACE	NASA TN D-645 CALCULATION OF WIND COMPENSATION FOR LAUNCHING OF UNGUIDED ROCKETS	NASA TN D-647 FATIGUE DAMAGE UNDER VARYING STRESS AMPLITUDES	Next

Bound With Nasa Tn D-641-642,644-650

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