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AU2003291694A8 - Device for establishing and sustaining laminar boundary-layer flow - Google Patents

Device for establishing and sustaining laminar boundary-layer flow

Info

Publication number
AU2003291694A8
AU2003291694A8 AU2003291694A AU2003291694A AU2003291694A8 AU 2003291694 A8 AU2003291694 A8 AU 2003291694A8 AU 2003291694 A AU2003291694 A AU 2003291694A AU 2003291694 A AU2003291694 A AU 2003291694A AU 2003291694 A8 AU2003291694 A8 AU 2003291694A8
Authority
AU
Australia
Prior art keywords
establishing
layer flow
laminar boundary
sustaining
sustaining laminar
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.)
Abandoned
Application number
AU2003291694A
Other versions
AU2003291694A1 (en
Inventor
Fabio Paolo Bertolotti
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of AU2003291694A8 publication Critical patent/AU2003291694A8/en
Publication of AU2003291694A1 publication Critical patent/AU2003291694A1/en
Abandoned 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
    • B64C21/02Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/44Varying camber
    • B64C3/46Varying camber by inflatable elements
    • 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)
  • Mechanical Engineering (AREA)
  • Nozzles (AREA)
AU2003291694A 2002-11-04 2003-11-03 Device for establishing and sustaining laminar boundary-layer flow Abandoned AU2003291694A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US42358702P 2002-11-04 2002-11-04
US60/423,587 2002-11-04
PCT/US2003/035003 WO2004041638A2 (en) 2002-11-04 2003-11-03 Device for establishing and sustaining laminar boundary-layer flow

Publications (2)

Publication Number Publication Date
AU2003291694A8 true AU2003291694A8 (en) 2004-06-07
AU2003291694A1 AU2003291694A1 (en) 2004-06-07

Family

ID=32312682

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003291694A Abandoned AU2003291694A1 (en) 2002-11-04 2003-11-03 Device for establishing and sustaining laminar boundary-layer flow

Country Status (2)

Country Link
AU (1) AU2003291694A1 (en)
WO (1) WO2004041638A2 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2427972A (en) * 1944-02-01 1947-09-23 Frederick C Melchior Self-energizing airfoil
US2841344A (en) * 1955-11-28 1958-07-01 Stroukoff Michael Boundary layer control
US5098037A (en) * 1989-11-06 1992-03-24 The B. F. Goodrich Company Structural airfoil having integral expulsive system

Also Published As

Publication number Publication date
WO2004041638A2 (en) 2004-05-21
AU2003291694A1 (en) 2004-06-07
WO2004041638A3 (en) 2004-08-19

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase