A Flight Investigation Of The Effects Of Compressibility On Applied Gust Loads
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Author | : Earle T. Binckley |
Publisher | : |
Total Pages | : 28 |
Release | : 1949 |
Genre | : Airplanes |
ISBN | : |
Download A Flight Investigation of the Effects of Compressibility on Applied Gust Loads Book in PDF, Epub and Kindle
Two jet-propelled airplanes were flow at different speeds in rough air to investigate the effects of compressibility on applied gust loads at Mach numbers up to 0.68. The results indicated that no compressibility correction to the slope of the lift curve was necessary.
Author | : Harry C. Mickleboro |
Publisher | : |
Total Pages | : 22 |
Release | : 1954 |
Genre | : |
ISBN | : |
Download A Flight Study of Compressibility Effects on the Gust Loads of a 35 Degree Sweptback-wing Airplane Book in PDF, Epub and Kindle
Author | : Harry C. Mickleboro |
Publisher | : |
Total Pages | : 25 |
Release | : 1954 |
Genre | : Airplanes |
ISBN | : |
Download A Flight Study of Compressibility Effects on the Gust Loads of a 35° Sweptback-wing Airplane Book in PDF, Epub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 970 |
Release | : 1955 |
Genre | : Aeronautics |
ISBN | : |
Download Technical Note - National Advisory Committee for Aeronautics Book in PDF, Epub and Kindle
Author | : John D. Stanitz |
Publisher | : |
Total Pages | : 712 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Download Two-dimensional Compressible Flow in Centrifugal Compressors with Straight Blades Book in PDF, Epub and Kindle
Six numerical examples are presented for steady, two-dimensional, compressible, nonviscous flow in centrifugal compressors with straight blades. A seventh example is presented for incompressible flow. The solutions also applye to radial-flow turbines with rotation and flow direction reversed. The effects of variations in following parameters were investigated: (1) flow rate, (2) impeller-tip speed, (3) variation of passage height with radius, and (4) number of blades. The numerical results are presented in plots of the streamlines, constant Mach number lines, and constant pressure-ratio lines. Correlation equations are developed whereby the flow conditions in any impeller with straight blades can be determined for all operating conditions.
Author | : |
Publisher | : |
Total Pages | : 506 |
Release | : 1952 |
Genre | : Aeronautics |
ISBN | : |
Download Technical Note Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1044 |
Release | : 1956 |
Genre | : Aeronautics |
ISBN | : |
Download Report Book in PDF, Epub and Kindle
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1640 |
Release | : 1956 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1654 |
Release | : 1949 |
Genre | : Government publications |
ISBN | : |
Download United States Government Publications Monthly Catalog Book in PDF, Epub and Kindle
Author | : Curt A. Holzhauer |
Publisher | : |
Total Pages | : 284 |
Release | : 1956 |
Genre | : Aerofoils |
ISBN | : |
Download Wind-tunnel and Flight Investigations of the Use of Leading-edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 ̊swept-wing Airplane Book in PDF, Epub and Kindle