Theoretical And Experimental Analysis Of The Reduction Of Rotor Blade Vibration In Turbomachinery Through The Use Of Modified Stator Vane Spacing
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Author | : Richard H. Kemp |
Publisher | : |
Total Pages | : 43 |
Release | : 1958 |
Genre | : Gas dynamics |
ISBN | : |
Experimental verification of the analysis was obtained by using an air-interrupter disk and comparing the vibration amplitudes of turbine blades in a turbojet engine when two different nozzle vane configurations were used. One was an equally spaced vane configuration, and the other was one which the analysis had indicated would result in a reduction of the excitation level. The measured amplitudes of vibration of the turbine blades during engine operation compared favorably with those predicted by the analysis.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 664 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 372 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 424 |
Release | : 1960 |
Genre | : |
ISBN | : |
Author | : United States. Dept. of Commerce. Office of Technical Services |
Publisher | : |
Total Pages | : 600 |
Release | : |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 638 |
Release | : 1959 |
Genre | : Science |
ISBN | : |
Author | : Patrick T. Chiarito |
Publisher | : |
Total Pages | : 38 |
Release | : 1960 |
Genre | : Vibration |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 382 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : Albert L. Braslow |
Publisher | : |
Total Pages | : 624 |
Release | : 1958 |
Genre | : Airplanes |
ISBN | : |
The method has been applied to various types of configurations in several wind-tunnel investigations conducted by the National Advisory Committee for Aeronautics at Mach numbers up to 4, and in all cases the calculated roughness height caused premature boundary-layer transition for the range of test conditions.
Author | : |
Publisher | : |
Total Pages | : 934 |
Release | : 1948 |
Genre | : Mechanics, Applied |
ISBN | : |