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SEMIEMPIRICAL PROCEDURE FOR ESTIMATING LIFT AND DRAG CHARACTERISTICS OF PROPELLER-WING-FLAP CONFIGURATIONS FOR VERTICAL-AND SHORT-TAKE-OFF-AND-LANDING AIRPLANES

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BookPublisher: Nasa, Washington, D.C. 1959Description: 38.DDC classification: NASA | MEMO 1-16-59L

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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 MEMO 1-16-59L (Browse shelf)	Not for loan		TR17733

Total holds: 0

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Previous	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)	NASA MEMO 1-18-59A - SUBSONIC WING LOADINGS ON A 45(DEGREE) SWEPTBACK-WING AND BODY COMBINATION AT HIGH ANGLES OF ATTACK	NASA MEMO 1-19-59A - FINISHING AND INSPECTION OF MODEL SURFACES BOUNDARY-LAYER-TRANSITION TESTS	Next

Bound With Nasa Memo 1-15-59l,1-17-59l-1-31-59l, Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l

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