DE69301141D1 - Steueranlagen der Grenzschicht - Google Patents

Steueranlagen der Grenzschicht

Info

Publication number
DE69301141D1
DE69301141D1 DE69301141T DE69301141T DE69301141D1 DE 69301141 D1 DE69301141 D1 DE 69301141D1 DE 69301141 T DE69301141 T DE 69301141T DE 69301141 T DE69301141 T DE 69301141T DE 69301141 D1 DE69301141 D1 DE 69301141D1
Authority
DE
Germany
Prior art keywords
control systems
boundary layer
boundary
layer
systems
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.)
Expired - Lifetime
Application number
DE69301141T
Other languages
English (en)
Inventor
Fouad Majdalawi
Ali Hasan Nayfeh
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by British Aerospace PLC filed Critical British Aerospace PLC
Application granted granted Critical
Publication of DE69301141D1 publication Critical patent/DE69301141D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C21/00Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
DE69301141T 1992-09-25 1993-09-27 Steueranlagen der Grenzschicht Expired - Lifetime DE69301141D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB929220250A GB9220250D0 (en) 1992-09-25 1992-09-25 Boundary layer control system

Publications (1)

Publication Number Publication Date
DE69301141D1 true DE69301141D1 (de) 1996-02-08

Family

ID=10722483

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69301141T Expired - Lifetime DE69301141D1 (de) 1992-09-25 1993-09-27 Steueranlagen der Grenzschicht

Country Status (3)

Country Link
EP (1) EP0589728B1 (de)
DE (1) DE69301141D1 (de)
GB (1) GB9220250D0 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6027078A (en) * 1998-02-27 2000-02-22 The Boeing Company Method and apparatus using localized heating for laminar flow
US7578483B1 (en) * 2000-10-12 2009-08-25 Oceanit Laboratories, Inc. Conformable skin element system for active vortex control
US9593670B2 (en) 2014-04-30 2017-03-14 General Electric Company System and methods for reducing wind turbine noise
US20160221664A1 (en) * 2015-01-30 2016-08-04 Hamilton Sundstrand Corporation Boundary layer control assembly for an aircraft airfoil and method of controlling a boundary layer
WO2024173703A1 (en) * 2023-02-15 2024-08-22 New Mexico Tech University Research Park Corporation Systems and methods for aircraft wing surfaces with aerodynamic patterns

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2943828A (en) * 1956-08-07 1960-07-05 North American Aviation Inc Thermal aerodynamic drag controller
US4932610A (en) * 1986-03-11 1990-06-12 The United States Of America As Represented By The United States National Aeronautics And Space Administration Active control of boundary layer transition and turbulence

Also Published As

Publication number Publication date
EP0589728B1 (de) 1995-12-27
EP0589728A1 (de) 1994-03-30
GB9220250D0 (en) 1993-01-06

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Legal Events

Date Code Title Description
8332 No legal effect for de