Analysis of Propeller Efficiency Losses Associated with Heated-air Thermal De-icing

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ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Analysis of Propeller Efficiency Losses Associated with Heated-air Thermal De-icing by : Blake W. Corson

Download or read book Analysis of Propeller Efficiency Losses Associated with Heated-air Thermal De-icing written by Blake W. Corson and published by . This book was released on 1946 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis is made of the loss of efficiency associated with a heated-air thermal de-icing propeller both with and without internal flow. For the available data, measured efficiency losses are compared with the calculated losses and the agreement is found to be within the experimental accuracy of the data. The method presented may be used with reasonable accuracy to determine the net change in propeller efficiency due to the combined effects of the nozzle and internal flow if the characteristics of the propeller without nozzles are known.

Technical Note - National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 1066 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1947 with total page 1066 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Index of NACA Technical Publications

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ISBN 13 :
Total Pages : 1370 pages
Book Rating : 4.3/5 (126 download)

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Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1949 with total page 1370 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Selected Listing of NASA Scientific and Technical Reports for ...

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ISBN 13 :
Total Pages : 664 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :

Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1949 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Report

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ISBN 13 :
Total Pages : 620 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Report by :

Download or read book Report written by and published by . This book was released on 1945 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Report - National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 516 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1946 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Annual Report of the National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 512 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Annual Report of the National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Annual Report of the National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1945 with total page 512 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Tank Tests to Determine the Effect of Varying Design Parameters of Planing-tail Hulls

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ISBN 13 :
Total Pages : 582 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Tank Tests to Determine the Effect of Varying Design Parameters of Planing-tail Hulls by : John R. Dawson

Download or read book Tank Tests to Determine the Effect of Varying Design Parameters of Planing-tail Hulls written by John R. Dawson and published by . This book was released on 1946 with total page 582 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second part of a series of tests made in Langley tank no. 2 to determine the effect of varying design parameters of planing-tail hulls is presented. Results are given to show the effects on resistance characteristics of varying angle of afterbody keel, depth of step, and length of afterbody chine. The effect of varying the gross load is shown for one configuration. The resistance characteristics of planing-tail hulls are compared withthose of a conventional flying-boat hull. The forces on the forebody and afterbody of one configuration are compared with the forces on a conventional hull.

Technical Note

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ISBN 13 :
Total Pages : 508 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Technical Note by :

Download or read book Technical Note written by and published by . This book was released on 1948 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of the Effect of a Tip Modification and Thermal De-icing Air Flow on Propeller Performance

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ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Investigation of the Effect of a Tip Modification and Thermal De-icing Air Flow on Propeller Performance by : Blake W. Corson

Download or read book Investigation of the Effect of a Tip Modification and Thermal De-icing Air Flow on Propeller Performance written by Blake W. Corson and published by . This book was released on 1946 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic tests of a 12.208-foot-diameter two-blade hollow steel propeller before and after alteration for thermal de-icing have been made in the Langley 16-foot high-speed tunnel to determine the effect of the alterations on propeller efficiency. The propeller, which had Clark Y blade sections, was tested on a 2000-horsepower dynamometer at blade angles ranging from about 25 degrees to 60 degrees at the 42-inch radius and at airspeeds varying from 100 to 425 miles per hour.

List of Technical Notes, 1947-1953

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ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis List of Technical Notes, 1947-1953 by : United States. National Advisory Committee for Aeronautics

Download or read book List of Technical Notes, 1947-1953 written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

United States Government Publications, a Monthly Catalog

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ISBN 13 :
Total Pages : 1808 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis United States Government Publications, a Monthly Catalog by : United States. Superintendent of Documents

Download or read book United States Government Publications, a Monthly Catalog written by United States. Superintendent of Documents and published by . This book was released on 1946 with total page 1808 pages. Available in PDF, EPUB and Kindle. Book excerpt: February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.

United States Government Publications Monthly Catalog

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ISBN 13 :
Total Pages : 1718 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis United States Government Publications Monthly Catalog by :

Download or read book United States Government Publications Monthly Catalog written by and published by . This book was released on 1946 with total page 1718 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Confidential Documents

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ISBN 13 :
Total Pages : 958 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Confidential Documents by : United States. Army Air Forces

Download or read book Confidential Documents written by United States. Army Air Forces and published by . This book was released on 1950 with total page 958 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Data Digest

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ISBN 13 :
Total Pages : 488 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Data Digest by :

Download or read book Technical Data Digest written by and published by . This book was released on 1950 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft

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ISBN 13 :
Total Pages : 492 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft by : Clifford J. Moore

Download or read book A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft written by Clifford J. Moore and published by . This book was released on 1970 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report investigates critical reviews of NACA and NASA report literature on light aircraft design, with emphasis on propulsion subsystems, stability, control, propellers, performance, and safety.

Apparent Effect of Inlet Temperature on Adiabatic Efficiency of Centrifugal Compressors

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ISBN 13 :
Total Pages : 644 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Apparent Effect of Inlet Temperature on Adiabatic Efficiency of Centrifugal Compressors by : Robert J. Anderson

Download or read book Apparent Effect of Inlet Temperature on Adiabatic Efficiency of Centrifugal Compressors written by Robert J. Anderson and published by . This book was released on 1948 with total page 644 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents results of investigation of apparent variation of centrifugal-compressor adiabatic efficiency with inlet temperature; effects of heat transfer and Reynolds number were considered.