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searching for Lifting-line theory 7 found (27 total)

alternate case: lifting-line theory

Drag count (388 words) [view diff] no match in snippet view article find links to article

Springer-Verlag. ISBN 978-3-642-57903-5. "Ask Us – Drag Coefficient & Lifting Line Theory". Aerospaceweb.org. 2004-07-11. Retrieved 2019-10-26. van Dam, C
Drag coefficient (2,716 words) [view diff] no match in snippet view article find links to article
Aircraft, Vol. 44, 2007, p. 824–32. "Ask Us – Drag Coefficient & Lifting Line Theory". Aerospaceweb.org. 2004-07-11. Retrieved 2010-12-07. "Boeing 787
Qian Xuesen (6,004 words) [view diff] no match in snippet view article find links to article
Aeronautical Sciences, 10(2): 68–70. 1945: (with Theodore von Kármán), "Lifting- line Theory for a Wing in Nonuniform Flow," Quarterly of Applied Mathematics
Swept wing (8,240 words) [view diff] no match in snippet view article find links to article
Jones in 1945. Sweep theory builds on other wing lift theories. Lifting line theory describes lift generated by a straight wing (a wing in which the
Wind-turbine aerodynamics (5,171 words) [view diff] no match in snippet view article find links to article
Reynolds-averaged Navier–Stokes equations. Free vortex models are similar to lifting line theory in that they assume that the wind turbine rotor is shedding either
John Joseph Montgomery (6,097 words) [view diff] exact match in snippet view article find links to article
what modern aerodynamicists refer to as a "circulation theory" or "lifting-line theory". Montgomery compiled his results into a 131-page manuscript titled
Theodore von Kármán bibliography (5,395 words) [view diff] exact match in snippet view article find links to article
ISSN 1533-385X. OCLC 809393. Kármán, Th. von; Tsien, H. S. (1945). "Lifting-line theory for a wing in non-uniform flow". Quarterly of Applied Mechanics.