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HOVERING CHARATERISTICS OF A ROTOR HAVING AN AIRFOIL SECTION DISIGNED FOR A UTILITY TYPE OF HELICOPTER

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BookPublisher: Nasa, Washington, D.C. 1962Description: 21.DDC classification: NASA | TN D-1517 -

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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-1517 - (Browse shelf)	Not for loan		TR8164

Total holds: 0

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Previous	NASA TN D-1514 - A STUDY ABORT FROM A MANNED LUNAR LANDING AND RETURN TO RENDEZVOUS IN A 50-MILE ORBIT	NASA TN D-1515 - SIMULATOR STUDY OF AN ACTIVE CONTROL SYSTEM FOR A SPINNING BODY	NASA TN D-1516 - SPIN INVESTIGATION OF A 1/20-SCALE MODEL OF ANSWEPT-WING,TWIN-ENGINE,OBSERVATION AIRPLANE	NASA TN D-1517 - HOVERING CHARATERISTICS OF A ROTOR HAVING AN AIRFOIL SECTION DISIGNED FOR A UTILITY TYPE OF HELICOPTER	NASA TN D-1518 - LONGITUDINAL AERODUNAMIC CHARACTERISTICS AT MACH NUMBERS FROM 0.40 TO 1.10 OF A BLUNTED RIGHT-TRIANGULAR PYRAMIDAL LIFTING REENTRY CONFIGURATION EMPLOYING VARIABLE-SWEEP WING PANELS	NASA TN D-1519 - THE EFFECT OF VACUUM ON THE PENETRATION CHARACTERISTICS OF PROJECTILES INTO FINE PARTICLES	NASA TN D-1520 - AN EXPERIMENTAL INVESTIGATION OF SEVERAL ABLATION MATARIALS IN AN ELECTRIC-ARC-HEATED AIR JET	Next

Bound With Nasa Tn D-1511-1520

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