Technical Note
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 372 |
| Release | : 1958 |
| Genre | : Aeronautics |
| ISBN | : |
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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Technical Note - National Advisory Committee for Aeronautics
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 664 |
| Release | : 1958 |
| Genre | : Aeronautics |
| ISBN | : |
Index of NACA Technical Publications
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 388 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
Simplified Method for Determination of Critical Height of Distributed Roughness for Boundary-layer Transition at Mach Numbers from 0 to 5
| 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.
Catalog of Technical Reports
| Author | : United States. Dept. of Commerce. Office of Technical Services |
| Publisher | : |
| Total Pages | : 600 |
| Release | : |
| Genre | : |
| ISBN | : |
Experimental Determination of the Temperature and Dynamic-strain Environment of a Tubular Combustor Liner in a Turbojet Engine
| Author | : Patrick T. Chiarito |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1960 |
| Genre | : Vibration |
| ISBN | : |
