A thrust equation treats propellers and rotors as aerodynamic cycles and calculates their thrust without resorting to the blade element method
<p>The lift generated by a translating wing of known translational speed, lift coefficient and area is calculated by a simple equation. A propeller or rotor generating thrust share the same aerodynamic principles but their different kinematics cause the calculation of their thrust to be laborious. T...
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| Formatua: | Artigo |
| Hizkuntza: | Inglês |
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Embry-Riddle Aeronautical University
2019-01-01
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| Saila: | International Journal of Aviation, Aeronautics, and Aerospace |
| Gaiak: | |
| Sarrera elektronikoa: | https://commons.erau.edu/ijaaa/vol6/iss5/9 |
| Etiketak: |
Etiketarik gabe, Izan zaitez lehena erregistro honi etiketa jartzen!
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