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.)) |
|---|---|
| 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): |
|
| Group: | GALCIT |
| Thesis Committee: |
|
| 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
![[img]](https://thesis.library.caltech.edu/style/images/fileicons/application_pdf.png)
|
PDF (Puckett_ae_1949.pdf)
- Final Version
See Usage Policy. 13MB |
Repository Staff Only: item control page
