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Analysis of high-aspect-ratio jet-flap wings of arbitrary geometry
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lissaman, P. B. S. |
| Copyright Year | 1973 |
| Description | An analytical technique to compute the performance of an arbitrary jet-flapped wing is developed. The solution technique is based on the method of Maskell and Spence in which the well-known lifting-line approach is coupled with an auxiliary equation providing the extra function needed in jet-flap theory. The present method is generalized to handle straight, uncambered wings of arbitrary planform, twist, and blowing (including unsymmetrical cases). An analytical procedure is developed for continuous variations in the above geometric data with special functions to exactly treat discontinuities in any of the geometric and blowing data. A rational theory for the effect of finite wing thickness is introduced as well as simplified concepts of effective aspect ratio for rapid estimation of performance. |
| File Size | 1571422 |
| Page Count | 59 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730008255 |
| Archival Resource Key | ark:/13960/t0wq4r04n |
| Language | English |
| Publisher Date | 1973-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Numerical Analysis Aerodynamic Configurations Wing Planforms Performance Prediction Jet Flaps Aerodynamic Characteristics Lift Augmentation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
