JP2006507188A5 - - Google Patents

Download PDF

Info

Publication number
JP2006507188A5
JP2006507188A5 JP2005501734A JP2005501734A JP2006507188A5 JP 2006507188 A5 JP2006507188 A5 JP 2006507188A5 JP 2005501734 A JP2005501734 A JP 2005501734A JP 2005501734 A JP2005501734 A JP 2005501734A JP 2006507188 A5 JP2006507188 A5 JP 2006507188A5
Authority
JP
Japan
Prior art keywords
synthetic jet
jet actuator
frequency
orifice
cavity
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP2005501734A
Other languages
English (en)
Japanese (ja)
Other versions
JP2006507188A (ja
Filing date
Publication date
Priority claimed from GB0313523A external-priority patent/GB0313523D0/en
Application filed filed Critical
Priority claimed from PCT/GB2004/002436 external-priority patent/WO2004110863A1/en
Publication of JP2006507188A publication Critical patent/JP2006507188A/ja
Publication of JP2006507188A5 publication Critical patent/JP2006507188A5/ja
Pending legal-status Critical Current

Links

JP2005501734A 2003-06-11 2004-06-09 渦破裂を制御する方法 Pending JP2006507188A (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP03253616 2003-06-11
GB0313523A GB0313523D0 (en) 2003-06-11 2003-06-11 Method of controlling vortex bursting
PCT/GB2004/002436 WO2004110863A1 (en) 2003-06-11 2004-06-09 Method of controlling vortex bursting

Publications (2)

Publication Number Publication Date
JP2006507188A JP2006507188A (ja) 2006-03-02
JP2006507188A5 true JP2006507188A5 (enExample) 2006-04-13

Family

ID=33553839

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2005501734A Pending JP2006507188A (ja) 2003-06-11 2004-06-09 渦破裂を制御する方法

Country Status (4)

Country Link
US (1) US20060145027A1 (enExample)
EP (1) EP1633625A1 (enExample)
JP (1) JP2006507188A (enExample)
WO (1) WO2004110863A1 (enExample)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8016244B2 (en) * 2004-02-20 2011-09-13 The Boeing Company Active systems and methods for controlling an airfoil vortex
GB0418196D0 (en) * 2004-08-14 2004-09-15 Rolls Royce Plc Boundary layer control arrangement
GB0420293D0 (en) 2004-09-10 2005-08-10 Bae Systems Plc Method of controlling vortex bursting
US20070029403A1 (en) * 2005-07-25 2007-02-08 The Boeing Company Dual point active flow control system for controlling air vehicle attitude during transonic flight
US7607470B2 (en) * 2005-11-14 2009-10-27 Nuventix, Inc. Synthetic jet heat pipe thermal management system
US8030886B2 (en) 2005-12-21 2011-10-04 Nuventix, Inc. Thermal management of batteries using synthetic jets
DE102010027081B4 (de) * 2010-07-13 2016-02-11 Deutsches Zentrum für Luft- und Raumfahrt e.V. Früherkennung eines Wirbelringstadiums
FR2968634B1 (fr) * 2010-12-08 2013-08-02 Snecma Pylone de fixation d'un moteur d'aeronef a helices propulsives non carenees
EP2676970B1 (en) 2012-06-22 2015-04-08 University Of Waterloo Hydrogenation of diene-based polymers
DE102015107626B4 (de) * 2015-05-15 2019-11-07 Airbus Defence and Space GmbH Strömungssteuerungsvorrichtung, Strömungsdynamischer Profilkörper und Strömungssteuerungsverfahren mit Schallwellenerzeugung
CN108860663B (zh) * 2018-07-24 2020-02-21 中国人民解放军国防科技大学 一种频率可控的自维持高速射流激励器

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4293110A (en) * 1979-03-08 1981-10-06 The Boeing Company Leading edge vortex flap for wings
US4626311A (en) * 1984-02-23 1986-12-02 Standard Textile Co., Inc. Cloth product having an antitheft device and method of making same
US4697769A (en) 1984-04-23 1987-10-06 Flow Industries, Inc. Method and apparatus for controlling bound vortices in the vicinity of lifting surfaces
GB2188397B (en) * 1984-09-13 1988-12-29 Rolls Royce A low drag surface construction
US4802642A (en) * 1986-10-14 1989-02-07 The Boeing Company Control of laminar flow in fluids by means of acoustic energy
DE3738366A1 (de) * 1987-11-12 1989-05-24 Deutsche Forsch Luft Raumfahrt Verfahren und vorrichtung zur erzeugung eines laminar-turbulenten grenzschichtuebergangs bei umstroemten koerpern
SE501139C2 (sv) * 1993-04-08 1994-11-21 Sem Ab Anordning vid fluidpump av membrantyp
US5647106A (en) * 1994-07-06 1997-07-15 Sensormatic Electronics Corporation Anti-theft system and method
US6457654B1 (en) * 1995-06-12 2002-10-01 Georgia Tech Research Corporation Micromachined synthetic jet actuators and applications thereof
US5758823A (en) * 1995-06-12 1998-06-02 Georgia Tech Research Corporation Synthetic jet actuator and applications thereof
US6821090B1 (en) * 1997-06-05 2004-11-23 Mcdonnell Douglas Helicopter Company Gust alleviation/flutter suppression device
US5945909A (en) * 1998-06-02 1999-08-31 B&G Plastics, Inc. Article identification and surveillance seal
US6138955A (en) * 1998-12-23 2000-10-31 Board Of Supervisors Of Louisiana State University And Agricultural And Mechanical College Vortical lift control over a highly swept wing
US6109566A (en) * 1999-02-25 2000-08-29 United Technologies Corporation Vibration-driven acoustic jet controlling boundary layer separation
US6412732B1 (en) * 1999-07-06 2002-07-02 Georgia Tech Research Corporation Apparatus and method for enhancement of aerodynamic performance by using pulse excitation control

Similar Documents

Publication Publication Date Title
JP2006507188A5 (enExample)
EP1863704B1 (en) Thrust generating apparatus
JP5231770B2 (ja) 航空機システム、およびエーロフォイルシステムを作動させるための方法
JP2016174940A5 (enExample)
JP2008538291A5 (enExample)
US8136767B2 (en) Method and system for flow control with arrays of dual bimorph synthetic jet fluidic actuators
JP2003056494A5 (enExample)
JP2015006620A5 (enExample)
US20060032988A1 (en) Boundary layer control arrangement
CN101454600A (zh) 改进的气体压力调节器
GB2474147A (en) Apparatus for stabilization and deceleration of supersonic flow incorporating a diverging nozzle and perforated plate
DE502006001063D1 (de) Kaltspritzanlage und Kaltspritzverfahren mit moduliertem Gasstrom
CN112156403B (zh) 一种压缩空气泡沫气液混合器及设计方法
SE541076C2 (sv) Ventilationsdon med ljuddämpning.
ES2155415A1 (es) Procedimiento para controlar modos de funcioonamiento de un aparato acondicionador de aire.
JP2006507188A (ja) 渦破裂を制御する方法
WO2009024101A3 (en) Aircraft, using a wall jet to create a lift for flight, with advanced controls of aircraft motion
WO2011004124A3 (fr) Microsystème de génération d'un jet synthétique, procédé de fabrication et dispositif de contrôle d'écoulement correspondants.
US3428258A (en) Open pore foam faucet insert
CN105857576A (zh) 基于喷流开口的降噪缝翼结构
CN104169090B (zh) 流体材料的连续喷射打印
Mair et al. Experimental and numerical analysis of a piezo driven fluidic device for active flow control
JP2007024421A (ja) ミスト発生方法及びその装置
RU2728577C2 (ru) Турбореактивный двухконтурный двигатель с раздельным истечением потоков из сопел
Sheng et al. Passive control of an offset attaching j et using a perforated plate