| タイトル | Theoretical investigations, and correlative studies for NLF, HLFC, and LFC swept wings at subsonic, transonic and supersonic speeds |
| 著者（英） | Goradia, S. H.; Harvey, W. D.; Bobbitt, P. J.; Ferris, J. C. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1987-10-01 |
| 言語 | eng |
| 内容記述 | Attention is given to the results of theory/experiment-correlation studies for natural laminar flow, LFC, and hybrid-LFC airfoils at subsonic and supersonic Mach numbers. The method of characteristics, integral compressible boundary layer methods for infinitely swept wings, and a method for prediction of separating turbulent boundary layer characteristics. The integral boundary layer methods are found to be successful at predicting both transonic and supersonic transition phenomena. Computations for wings with 0-50 deg sweep angle, Reynolds number range of 1-30 million, and with and without LFC, are in good agreement with experimental data. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 88A38950
SAE PAPER 871861 |
| 権利 | Copyright |
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