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AERODYNAMIC DAMPING AND OSCILLATORY STABILITY IN PITCH FOR A MODEL OF A TYPICAL SUBSONIC JET-TRANSPORY AIRPLANE

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BookPublisher: Nasa, Washington, D.C. 1966Description: 14.DDC classification: NASA | TN D-3159

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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-3159 (Browse shelf)	Not for loan		TR15214

Total holds: 0

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Previous	NASA TN D-3156 PRESSURE FLUCTUATIONS IN TURBULENT BOUNDARY LAYERS	NASA TN D-3157 TEST OF A TRUSS-CORE SANDWICH CYLINDER LOADED TO FAILURE IN BENDING	NASA TN D-3158 AN APPROXIMATE METHOD FOR SOLVING THE SINGLE-DEGREE-OF-FREEDOM ROLL EQUATION WITH TIME-DEPENDENT COEFFICIENTS	NASA TN D-3159 AERODYNAMIC DAMPING AND OSCILLATORY STABILITY IN PITCH FOR A MODEL OF A TYPICAL SUBSONIC JET-TRANSPORY AIRPLANE	NASA TN D-3160 ATOMIC BEAM DETERMINATION OF THE CESIUM-CESIUM TOTAL SCATTERING CROSS SECTION	NASA TN D-3162 - STRUCTURAL CONCEPTS FOR HYDROGEN-FUELED HYPERSONIC AIRPLANES	NASA TN D-3182 STATIC AERODYNAMIC CHARACTERISTICS OF A ROCKET VEHICLE WITH THICK WEDGE FINS AND SWEPTBACK LEADING AND TRALING EDGES	Next

Bound With Nasa Tn D-3151-58,3160

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