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EVALUATION OF AN AEROELASTIC MODEL TECHNIQUE FOR PREDICTING AIRPLANE BUFFET LOADS

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BookPublisher: Nasa, Washington, D.C. 1973Description: 60.DDC classification: NASA | TN D-7066

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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-7066 (Browse shelf)	Not for loan		TR12749

Total holds: 0

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Previous	NASA TN D-7063 OPERATIONAL FREQUENCY STABILITY OF RUBIDIUM AND CESIUM FREQUENCY STANDARDS	NASA TN D-7064 MEASURED MICROWAVE SCATTERING CROSS SECTIONS OF THREE METEORITE SPECIMENS	NASA TN D-7065 A STEP IN TIME	NASA TN D-7066 EVALUATION OF AN AEROELASTIC MODEL TECHNIQUE FOR PREDICTING AIRPLANE BUFFET LOADS	NASA TN D-7067 AN ACTUATOR EXTENSION TRANSFORMATION FOR A MOTION SIMULATOR AND AN INVERSE TRANSFORMATION APPLYING NEWTON-RAPHSON'S METHODS	NASA TN D-7068 NUMERICAL METHOD FOR THE SOLUTION OF LARGE SYSTEMS OF DIFFERENTIAL EQUATIONS OF THE BOUNDARY-LAYER TYPE	NASA TN D-7069 AERODYNAMIC CHARACTERISTICS OF A SWEPT-WING CRUISE MISSILE AT MACH NUMBERS FROM 0.50 TO 2.86	Next

Bound With Nasa Tn D- 7060-7065,7067-7069

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