Citation
Puckett, Allen Emerson (1949) Supersonic Wave Drag of Thin Airfoils. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/HYJJ-3241. https://resolver.caltech.edu/CaltechETD:etd-06232004-141931
Abstract
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.
Item Type: | Thesis (Dissertation (Ph.D.)) |
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Subject Keywords: | airfoils ; (Aeronautics and Mathematics) |
Degree Grantor: | California Institute of Technology |
Division: | Engineering and Applied Science |
Major Option: | Aeronautics |
Minor Option: | Mathematics |
Thesis Availability: | Public (worldwide access) |
Research Advisor(s): |
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Group: | GALCIT |
Thesis Committee: |
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Defense Date: | 1 January 1949 |
Record Number: | CaltechETD:etd-06232004-141931 |
Persistent URL: | https://resolver.caltech.edu/CaltechETD:etd-06232004-141931 |
DOI: | 10.7907/HYJJ-3241 |
Default Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. |
ID Code: | 2697 |
Collection: | CaltechTHESIS |
Deposited By: | Imported from ETD-db |
Deposited On: | 24 Jun 2004 |
Last Modified: | 29 Mar 2023 16:49 |
Thesis Files
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PDF (Puckett_ae_1949.pdf)
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