Drag divergence Mach number
Results: 4
| # | Item |
|---|---|
1 | MACH NUMBER, RELATIVE THICKNESS, SWEEP AND LIFT COEFFICIENT OF THE WING – AN EMPIRICAL INVESTIGATION OF PARAMETERS AND EQUATIONS D. Scholz, S. Ciornei Hamburg University of Applied Sciences Department of Automotive andAdd to Reading ListSource URL: www.fzt.haw-hamburg.deLanguage: English - Date: 2005-10-26 05:29:51 |
2 | Mach Number, Relative Thickness, Luftund Sweep andDeutscher Lift Coefficient of the WingAdd to Reading ListSource URL: www.fzt.haw-hamburg.deLanguage: English - Date: 2005-10-26 05:29:08 |
3![TF-8A Crusader with Supercritical Wing NASA Conference Publication[removed]Justin Murtha, John Stephens,](https://www.pdfsearch.io/img/7d7c0e237f913fa54bf0a0b40bd09008.jpg "TF-8A Crusader with Supercritical Wing NASA Conference Publication[removed]Justin Murtha, John Stephens,") | TF-8A Crusader with Supercritical Wing NASA Conference Publication[removed]Justin Murtha, John Stephens,Add to Reading ListSource URL: www.logbookmag.comLanguage: English - Date: 2012-02-24 02:11:55 |
4 | NASA Technical PaperAdd to Reading ListSource URL: www.southampton.ac.ukLanguage: English - Date: 2006-12-04 07:30:46 |