Experimental evaluation of sinusoidal leading edges

被引：194

作者：

Miklosovic, David S. ^{[1
]}

Murray, Mark M.

Howle, Laurens E.

机构：

[1] USN Acad, Dept Aerosp Engn, Annapolis, MD 21402 USA

[2] Duke Univ, Dept Mech Engn, Durham, NC 27708 USA

来源：

JOURNAL OF AIRCRAFT | 2007年 / 44卷 / 04期

关键词：

D O I：

10.2514/1.30303

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1404 / 1408

页数：5

共 12 条

[1]

Barlow J. B., 1999, Low Speed Wind Tunnel Testing, V3rd

[2]

Bethwaite F., 1993, HIGH PERFORMANCE SAI

[3]

Drela M., 2001, Xfoil 6.94 user guide

[4] HYDRODYNAMIC-DESIGN OF THE HUMPBACK WHALE FLIPPER [J].

FISH, FE ;

BATTLE, JM .

JOURNAL OF MORPHOLOGY, 1995, 225 (01) :51-60

[5] Influence of trailing-edge flow control on airfoil performance [J].

Gai, SL ;

Palfrey, R .

JOURNAL OF AIRCRAFT, 2003, 40 (02) :332-337

[6]

Hansen M.O., 2000, Aerodynamics of Wind Turbines: Rotors, Loads and Structure, VVolume 17

[7]

LAMAR JE, 1982, TM83303 NASA

[8]

LEVSHIN A, 2006, 20062868 AIAA

[9] Leading-edge tubercles delay stall on humpback whale (Megaptera novaeangliae) flippers [J].

Miklosovic, DS ;

Murray, MM ;

Howle, LE ;

Fish, FE .

PHYSICS OF FLUIDS, 2004, 16 (05) :L39-L42

[10] EXPERIMENTAL STUDIES OF SEPARATION ON A TWO-DIMENSIONAL AIRFOIL AT LOW REYNOLDS-NUMBERS [J].

MUELLER, TJ ;

BATILL, SM .

AIAA JOURNAL, 1982, 20 (04) :457-463

← 1 2 →