学位论文详细信息
Supersonic wave drag of thin airfoils | |
airfoils;Aeronautics | |
Puckett, Allen E. ; von Kármán, Theodore | |
University:California Institute of Technology | |
Department:Engineering and Applied Science | |
关键词: airfoils; Aeronautics; | |
Others : https://thesis.library.caltech.edu/2697/1/Puckett_ae_1949.pdf | |
美国|英语 | |
来源: Caltech THESIS | |
【 摘 要 】
The linearization of the equations of motion for the supersonic flow of a perfect fluid is discussed, and methods of solution using elementary source sink solutions are developed. These methods are applied to the calculation of performance of several types of three-dimensional supersonic airfoils; in particular, the drag at zero lift of a family of almost triangular, symmetrical wings is calculated. The significance of the results is discussed.
【 预 览 】
Files | Size | Format | View |
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Supersonic wave drag of thin airfoils | 13328KB | download |