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WIND-TUNNEL MEASUREMENT OF PROPELLER WHIRL-FLUTTER SPEEDS AND STATIC-STABILITY DERIVATIVES AND AOMPARISON WITH THEORY.

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BookPublisher: Nasa, Washington, D.C. 1963Description: 53.DDC classification: NASA | TN D-1807

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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-1807 (Browse shelf)	Not for loan		TR15510

Total holds: 0

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Previous	NASA TN D-1795 - COMPARISON OF EXPERIMENTAL AND THEORETICAL RESULTS FOR THE COMPRESSIBLE TURBULENT-BOUNDARY-LAYER SKIN FRICTION WITH ZERO PRESSURE GRADIENT	NASA TN D-1803 INVESTIGATION OF THE EFFECTS OF VARIABLE-AMPLITUDE LOADINGS ON FATIGUE CRACK PROPGATION PATTERNS.	NASA TN D-1804 PERFORMANCE OF A PLUG NOZZLE HAVING A CONCAVE CENTRAL BASE WITH AND WITHOUT TERMINAL FAIRINGS AT TRANSONIC SPEEDS.	NASA TN D-1807 WIND-TUNNEL MEASUREMENT OF PROPELLER WHIRL-FLUTTER SPEEDS AND STATIC-STABILITY DERIVATIVES AND AOMPARISON WITH THEORY.	NASA TN D-182 INVESTIGATION OF IGNITION TEMERATURES OF SOLID METALS	NASA TN D-183 EFFECTS OF A LOWER SURFACE JET ON THE LIFT-DRAG RATIO OF A 45 DEGREE SWETBACK AT A MACH NUMBER OF 2.01	NASA TN D-1832 NASA TN [D-1832]	Next

Bound With Nasa Tn D-1801-1806,1808-1810.Lack No-1805

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