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EBookClubs

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Book NASA Technical Note

Download or read book NASA Technical Note written by and published by . This book was released on 1963 with total page 902 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Propeller Slipstream Effects as Determined from Wing Pressure Distribution on a Large scale Six propeller VTOL Model at Static Thrust

Download or read book Propeller Slipstream Effects as Determined from Wing Pressure Distribution on a Large scale Six propeller VTOL Model at Static Thrust written by Matthew M. Winston and published by . This book was released on 1962 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aeronautical Report

Download or read book Aeronautical Report written by National Research Council Canada and published by . This book was released on 1960 with total page 1320 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wing Pressure Measurements Within the Propeller Slipstream for a Large scale V STOL Wind tunnel Model Simulating Transition

Download or read book Wing Pressure Measurements Within the Propeller Slipstream for a Large scale V STOL Wind tunnel Model Simulating Transition written by Matthew M. Winston and published by . This book was released on 1963 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book U S  Government Research Reports

Download or read book U S Government Research Reports written by and published by . This book was released on 1961 with total page 1116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Publications of the Division of Mechanical Engineering and the National Aeronautical Establishment

Download or read book Publications of the Division of Mechanical Engineering and the National Aeronautical Establishment written by National Research Council Canada. Division of Mechanical Engineering and published by . This book was released on 1965 with total page 352 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Data from a Static thrust Investigation of a Large scale General Research Vtol stol Model in Ground Effect

Download or read book Data from a Static thrust Investigation of a Large scale General Research Vtol stol Model in Ground Effect written by Robert J. Huston and published by . This book was released on 1960 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller diameters above the ground. The slipstream of the propellers was deflected by tilting the wing and propellers, by deflections of large-chord trailing-edge flaps, and by combinations of flap deflection and wing tilt. Tests were conducted over a range of propeller disk loadings from 7.41 to 29.70 pounds per square foot. Force data for the complete model and pressure distributions for the wing and flaps behind one propeller were recorded and are presented in tabular form without analysis.

Book Journal of the Royal Aeronautical Society

Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1966 with total page 1304 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Contractor Report

Download or read book NASA Contractor Report written by and published by . This book was released on 1985 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1963 with total page 1196 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Journal of the Royal Aeronautical Society

Download or read book The Journal of the Royal Aeronautical Society written by Royal Aeronautical Society and published by . This book was released on 1963 with total page 1168 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Propeller Propulsion System Integration

Download or read book Propeller Propulsion System Integration written by Stan J. Miley and published by . This book was released on 1985 with total page 194 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Propeller Propulsion System Integration

Download or read book Propeller Propulsion System Integration written by S. J. Miley and published by . This book was released on 1985 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt: A literature survey was performed to identify and review technical material applicable to the problem area of propeller propulsion system integration. The survey covered only aerodynamic interference aspects of the problem, and was restricted primarily to propeller effects on the airframe. The subject of airframe aerodynamic interference on the propeller was limited to the problem of vibration due to nonuniform inflow. The problem of airframe effects on propeller performance was not included. A total of 1121 references are given. The references are grouped into the subject areas of Aircraft Stability, Propulsive Efficiency, Aerodynamic Interference, Aerodynamic Interference-Propeller Vibration, and Miscellaneous.

Book Further Measurements of Model Propeller Pressure Distributions Using a Novel Technique

Download or read book Further Measurements of Model Propeller Pressure Distributions Using a Novel Technique written by Stuart D. Jessup and published by . This book was released on 1986 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: Model propeller blade pressure distributions were measured using a novel technique. A single pressure gage was installed at a radial position to measure pressures at numerous chordwise locations through pressure taps and connecting channels. The technique resulted in accurate, detailed pressure distributions along two radial positions using two pressure gages. The major advantage of this technique is the ability to make measurements in the thin parts of the blade with high potential accuracy, and no disruption to the measuring surface, except for the orifice hole. The relatively along test time required to collect the data is the disadvantage. Keywords: Marine Propeller, Propeller Research Pressure Distribution, Model Experiments.