General approach to lifting-line theory, applied to wings with sweep

被引：0

作者：

Reid, Jackson T. ^{[1
]}

Hunsaker, Douglas F. ^{[1
]}

机构：

[1] Utah State University, Logan,UT,84321, United States

来源：

Journal of Aircraft | 2021年 / 58卷 / 02期

关键词：

38;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：334 / 346

共 50 条

[41] UNSTEADY LIFTING-LINE THEORY AS A SINGULAR-PERTURBATION PROBLEM
AHMADI, AR
WIDNALL, SE
JOURNAL OF FLUID MECHANICS, 1985, 153 (APR) : 59 - 81
[42] LIFTING SURFACE THEORY APPLIED TO FIXED WINGS AND PROPELLERS
DAT, R
RECHERCHE AEROSPATIALE, 1973, (04): : 245 - 254
[43] Analytical decomposition of wing roll and flapping using lifting-line theory
Phillips, W.F., 1600, AIAA International (51):
[44] UNSTEADY LIFTING-LINE THEORY AS A SINGULAR-PERTURBATION PROBLEM.
Ahmadi, Ali R.
Widnall, Sheila E.
Journal of Fluid Mechanics, 1985, 153 : 59 - 81
[45] Analytical Decomposition of Wing Roll and Flapping Using Lifting-Line Theory
Phillips, W. F.
JOURNAL OF AIRCRAFT, 2014, 51 (03): : 761 - 778
[46] An approach for unsteady lifting-line time-marching numerical computation
Devinant, P
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 1998, 26 (02) : 177 - 197
[47] A lifting-line theory and a critical shear Parameter of a wing in uniform shear flow
Ito, Jun
Nakamura, Goh
Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 2003, 69 (679): : 547 - 552
[48] THE THEORY OF OSCILLATING THICK WINGS IN SUBSONIC FLOW - LIFTING LINE THEORY
DRAGOS, L
ACTA MECHANICA, 1985, 54 (3-4) : 221 - 238
[49] LIFTING-LINE THEORY OF SUPERCAVITATING PROPELLERS AT NON-ZERO CAVITATION NUMBERS
NISHIYAM.T
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1971, 51 (08): : 577 - &
[50] Stall Recovery of a Morphing Wing via Extended Nonlinear Lifting-Line Theory
Gamble, Lawren L.
Pankonien, Alexander M.
Inman, Daniel J.
AIAA JOURNAL, 2017, 55 (09) : 2956 - 2963

← 1 2 3 4 5 →