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An Experimental Investigation Of The Normal Acceleration Of An Airplane Model In A Gust
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Book Synopsis An Experimental Investigation of the Normal Acceleration of an Airplane Model in a Gust by : Philip Donely
Download or read book An Experimental Investigation of the Normal Acceleration of an Airplane Model in a Gust written by Philip Donely and published by . This book was released on 1939 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: The investigation also shows that the value of maximum lift coefficient for steady flow does not limit the acceleration increment in a gust.
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 1949 with total page 870 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms by : Max A. Heaslet
Download or read book The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms written by Max A. Heaslet and published by . This book was released on 1948 with total page 726 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
Download or read book Technical Note written by and published by . This book was released on 1947 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Experiments on the Simulation of Gusts in a Wind Tunnel by : Arnold Martin Kuethe
Download or read book Preliminary Experiments on the Simulation of Gusts in a Wind Tunnel written by Arnold Martin Kuethe and published by . This book was released on 1955 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Combined Beam-column Stresses of Aluminum-alloy Channel Sections by : R. Gottlieb
Download or read book Combined Beam-column Stresses of Aluminum-alloy Channel Sections written by R. Gottlieb and published by . This book was released on 1939 with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of a research program to obtain design data on the strength of open-channel aluminum-alloy sections subjected to combined column and beam action.
Book Synopsis Standard Procedures for Rating and Testing Multistage Axial-flow Compressors by : United States. National Advisory Committee for Aeronautics
Download or read book Standard Procedures for Rating and Testing Multistage Axial-flow Compressors written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1946 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt: In order to establish a standard procedure for rating and testing multistage axial-flow compressors, the NACA Subcommittee on Compressors appointed a panel to write such a procedure. This panel made recommendations for standardization of test setups, instrumentation, test procedure, data to be taken, and the presentation of the data. These recommendations are presented.
Book Synopsis Calculation of Tunnel-induced Upwash Velocities for Swept and Yawed Wings by : S. Katzoff
Download or read book Calculation of Tunnel-induced Upwash Velocities for Swept and Yawed Wings written by S. Katzoff and published by . This book was released on 1948 with total page 670 pages. Available in PDF, EPUB and Kindle. Book excerpt: The tunnel-induced upwash for a wing of any plan form and load distribution in a rectangular tunnel may be found with the aid of only two charts. One is given in the present paper. The second must be computed for each tunnel. The second chart is given for an open tunnel of 2:1 width-height ratio, a closed tunnel of 2:5 width-height ratio, and a closed tunnel of 10:7 width-height ratio.
Book Synopsis Physical Properties of Synthetic Resin Materials by : Meyer Fishbein
Download or read book Physical Properties of Synthetic Resin Materials written by Meyer Fishbein and published by . This book was released on 1939 with total page 562 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was made to determine the physical properties of synthetic resins having paper, canvas, and linen reinforcements, and of laminated wood impregnated with a resin varnish.
Book Synopsis Catalogue of the Public Documents of the ... Congress and of All Departments of the Government of the United States for the Period from ... to ... by : United States. Superintendent of Documents
Download or read book Catalogue of the Public Documents of the ... Congress and of All Departments of the Government of the United States for the Period from ... to ... written by United States. Superintendent of Documents and published by . This book was released on with total page 2868 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Annual Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Annual Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
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 1939 with total page 780 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
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 1953 with total page 274 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Further Experiments on the Flow and Heat Transfer in a Heated Turbulent Air Jet by : Alfred Gessow
Download or read book Further Experiments on the Flow and Heat Transfer in a Heated Turbulent Air Jet written by Alfred Gessow and published by . This book was released on 1950 with total page 304 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report by : United States. National Advisory Committee for Aeronautics
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1950 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Investigation in Climb and at High Speed Or a Two-blade and Three-blade Propeller by : Jerome B. Hammack
Download or read book Flight Investigation in Climb and at High Speed Or a Two-blade and Three-blade Propeller written by Jerome B. Hammack and published by . This book was released on 1949 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains the results obtained with a propeller in a three-blade and two-blade configuration in climb and high-speed flight when mounted on a slender-nose fighter airplane. An extensive series of power loadings were investigated up to an airplane Mach number of 0.7. The results are explained by theory. Recommendations for propeller efficiency improvement are stated.
