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A NOTE ON THE CALCULATION OF HELICOPTER PERFORMANCE AT HIGH TIP-SPEED RATIOS.

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BookPublisher: Nasa, Washington, D.C. 1959Description: 13.DDC classification: NASA | TN D-97

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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-97 (Browse shelf)	Not for loan		TR15738

Total holds: 0

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Previous	NASA TN D-967 MEASUREMENT AND EMPIRICAL CORRELATION OF TRANSPIRATION-COOLING PARAMETERS ON A 25 (DEGREE) CONE IN A TURBULENT BOUNDARY LAYER IN BOTH FREE FLIGHT AND HOT-GAS JET	NASA TN D-968 CHARTS DEPICTING KINEMATIC AND HEATING PARAMETERS FOR A BALLISTIC REENTRY AT SPEEDS OF 26,000 TO 45,000 FEET PER SECOND	NASA TN D-969 EFFECT OF GROUNDBOARD HEIGHT ON THE AERODYNAMIC CHARACTERISTICS OF A LIFTING CIRCULARY CYLINDER USING TANGENTIAL BLOWING FROM SURFACE SLOTS FOR LIFT GENERATION	NASA TN D-97 A NOTE ON THE CALCULATION OF HELICOPTER PERFORMANCE AT HIGH TIP-SPEED RATIOS.	NASA TN D-970 EFFECT OF GROUND PROXIMITY ON THE AERODYNAMIC CHARACTERISTICS OF ASPECT-RATIO-1 AIRFOILS WITH AND WITHOUT END PLATES	NASA TN D-98 OPTIMUM PROPORTIONS OF TRUSS-CORE AND WEB-CORE SANDWICH PLATES LOADED IN COMPRESSION.	NASA TN D-982 - TAKE-OFF DISTANCES OF A SUPERSONIC TRANSPORT CONFIGURATION AS AFFECTED BY AIRPLANE ROTATION DURING THE TAKE-OFF RUN	Next

Bound With Nasa Tn D-91-96,98-100.

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