Normal view MARC view ISBD view

ANALYTICAL AND EXPERIMENTAL DETERMINATION OF THE COUPLED NATURAL FREQUENCIES AND MODE SHAPES OF A DYNAMIC MODEL OF A SINGLE-ROTOR HELICOPTER

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1958Description: 42.DDC classification: NASA | MEMO 11-5-58L -

average rating: 0.0 (0 votes)

Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA MEMO 11-5-58L - (Browse shelf)	Not for loan		TR7925

Total holds: 0

Previous								Next
Previous	NASA MEMO 1-10-59A - TWO-DIMENSIONAL, SUPERSONIC, LINEARIZED FLOW WITH HEAT ADDITION	NASA MEMO 1-10-59L - HYDROGEN PEROXIDE HOT-JET SIMULATOR FOR WIND-TUNNEL TESTS OF TURBOJET-EXIT MODELS	NASA MEMO 11-4-58L - FLIGHT INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A 1/4-SCALE MODEL OF A TILT WING VERTICAL-TAKE OFF-AND-LANDING AIRCRAFT	NASA MEMO 11-5-58L - ANALYTICAL AND EXPERIMENTAL DETERMINATION OF THE COUPLED NATURAL FREQUENCIES AND MODE SHAPES OF A DYNAMIC MODEL OF A SINGLE-ROTOR HELICOPTER	NASA MEMO 1-16-59A - NUMERICAL METHOD FOR CALCULATING THE WAVE DRAG OF A CONFIGURATION FROM THE SECOND DERIVATIVE OF THE AREA DISTRIBUTION OF A SERIES OF EQUIVALENT BODIES OF REVOLUTION	NASA MEMO 1-16-59L SEMIEMPIRICAL PROCEDURE FOR ESTIMATING LIFT AND DRAG CHARACTERISTICS OF PROPELLER-WING-FLAP CONFIGURATIONS FOR VERTICAL-AND SHORT-TAKE-OFF-AND-LANDING AIRPLANES	NASA MEMO 1-17-59A - ESTIMATION OF STATIC LONGITUDINAL STABILITY OF AIRCRAFT CONFIGURATIONS AT HIGH MACH NUMBERS AND AT ANGLES OF ATTACK BETWEEN 0(DEGREE) AND +-180(DEGREE)	Next

Bound With Nasa Memo 11-3-58l-11-5-58l

There are no comments for this item.

PKK Library