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PROPELLER SLIPSTREAM EFFECTS AS DETERMINED FROM WING PRESSURE DISTRIBUTION ON A LARGE-SCALE SIX-PROPELLER VTOL MODEL AT STATIC THRUST

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BookPublisher: Nasa, Washington, D.C. 1962Description: 67.DDC classification: NASA | TN D-1509

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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-1509 (Browse shelf)	Not for loan Untraceable		TR11473

Total holds: 0

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Previous	NASA TN D-1506 STABILITY INVESTIGATION OF A BLUNTED CONE AND A BLUNTED OGIVE WITH A FLARED CYLINDER AFTERBODY AT MACH NUMBERS FROM 0.30 TO 2.85	NASA TN D-1507 PRESSURE DISTRIBUTION INDUCED ON A FLAT PLATE AT A FREE-STREAM MACH NUMBER OF 1.39 BY ROCKETS EXHAUSTING UPSTREAM AND DOWNSTREAM	NASA TN D-1508 STATIC STABILITY TESTS IN THE LANGLEY 24-INCH HYPERSONIC ARC TUNNEL ON A BLUNTED CONE AT MACH NUMBER OF 20	NASA TN D-1509 PROPELLER SLIPSTREAM EFFECTS AS DETERMINED FROM WING PRESSURE DISTRIBUTION ON A LARGE-SCALE SIX-PROPELLER VTOL MODEL AT STATIC THRUST	NASA TN D-1512 - THE INFLUENCE OF PRECESSION OF EARTH RENDEZVOUS ORBIT ON LUNAR MISSION REQUIREMENTS	NASA TN D-1513 - BUCKLING OF RING-STIFFENED CYLINDERS UNDER A PURE BENDING MOMENT AND A NONUNIFORM TEMPERATURE DISTRIBUTION	NASA TN D-1514 - A STUDY ABORT FROM A MANNED LUNAR LANDING AND RETURN TO RENDEZVOUS IN A 50-MILE ORBIT	Next

Bound With Nasa Tn D-1501-1508.

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