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METHOD FOR DETERMINING NORMAL MODES AND FREQUENCIES OF A LAUNCH VEHICLE UTILIZING ITS COMPONENT NORMAL MODES [NASA TN D-4550]

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Material type: Text

TextLanguage: English Publication details: National Aeronautics and Space Administration 1968 Washington, D.C.Description: 49pSubject(s):

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Holdings
Item type	Current library	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D 4541-4550	Not for loan		TR016150

Total holds: 0

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Previous	ON THE COSTRUCTION OF HIGHLY STABLE, EXLICT, NUMERICAL METHODS FOR INTGERATING COUPLED ORDINARY DIFFERENTIAL EQUATIONS WITH PARASITIC EIGENVALUES [NASA TN D-4547]	THE EFFECT OF INTERFIBER DISTANCE AND TEMERATURE ON THE CRITICAL ASPECT RATIO IN COMPOSITES [NASA TN D-4548]	APPLICATION OF MAXIMUM LIKELIHOOD TECHNIQUES TO THE DESIGN OF OPTIMUM STAR TRACKERS [NASA TN D-4549]	METHOD FOR DETERMINING NORMAL MODES AND FREQUENCIES OF A LAUNCH VEHICLE UTILIZING ITS COMPONENT NORMAL MODES [NASA TN D-4550]	NASA Technical Note [NASA TN D-5044]: Fortran program for calculating velocities and streamlines on a blade-to-blade stream surface of a tandem blade turbomachine	NASA Technical Note [NASA TN D-5046]: A method for determining the total drag of a pointed body of revolution in supersonic flow with turbulent boundary layer	NASA Technical Note [NASA TN D-5047]: Full-scale investigation of the aerodynamic characteristics of a sailwing of aspect ratio 5.9	Next

Bound vol. contains NASA TN D 4541-4550

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