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AU2002227282A1 - Joined wing supersonic aircraft - Google Patents

Joined wing supersonic aircraft

Info

Publication number
AU2002227282A1
AU2002227282A1 AU2002227282A AU2728202A AU2002227282A1 AU 2002227282 A1 AU2002227282 A1 AU 2002227282A1 AU 2002227282 A AU2002227282 A AU 2002227282A AU 2728202 A AU2728202 A AU 2728202A AU 2002227282 A1 AU2002227282 A1 AU 2002227282A1
Authority
AU
Australia
Prior art keywords
supersonic aircraft
joined wing
wing supersonic
joined
aircraft
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
AU2002227282A
Inventor
John M. Morgenstern
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.)
Lockheed Martin Corp
Original Assignee
Lockheed Corp
Lockheed Martin Corp
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 Lockheed Corp, Lockheed Martin Corp filed Critical Lockheed Corp
Publication of AU2002227282A1 publication Critical patent/AU2002227282A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B64C39/068—Aircraft not otherwise provided for having disc- or ring-shaped wings having multiple wings joined at the tips
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
AU2002227282A 2000-12-08 2001-12-06 Joined wing supersonic aircraft Abandoned AU2002227282A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US25176000P 2000-12-08 2000-12-08
US60/251,760 2000-12-08
PCT/US2001/046993 WO2002046038A2 (en) 2000-12-08 2001-12-06 Joined wing supersonic aircraft

Publications (1)

Publication Number Publication Date
AU2002227282A1 true AU2002227282A1 (en) 2002-06-18

Family

ID=22953288

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2002227282A Abandoned AU2002227282A1 (en) 2000-12-08 2001-12-06 Joined wing supersonic aircraft

Country Status (4)

Country Link
US (1) US6729577B2 (en)
EP (1) EP1347915A2 (en)
AU (1) AU2002227282A1 (en)
WO (1) WO2002046038A2 (en)

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US20050116107A1 (en) * 2003-11-11 2005-06-02 Supersonic Aerospace International, Llc Area ruling for vertical stabilizers
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US20060060696A1 (en) * 2004-08-26 2006-03-23 Cordy Clifford B Jr Link between the wing and canard for flutter reduction
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US7828243B2 (en) * 2005-08-03 2010-11-09 Northrop Grumman Systems Corporation SCRAMjet arrangement for hypersonic aircraft
US7410122B2 (en) * 2006-03-20 2008-08-12 The Boeing Company VTOL UAV with lift fans in joined wings
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US7302839B1 (en) 2006-06-22 2007-12-04 Cessna Aircraft Company Method and system for gathering pressure signature data using a scaled model in a wind tunnel
US7946535B2 (en) * 2006-10-18 2011-05-24 Aerion Corporation Highly efficient supersonic laminar flow wing
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US20080105783A1 (en) * 2006-11-03 2008-05-08 Cessna Aircraft Company Fuselage design for sonic boom suppression of supersonic aircraft
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FR2909359B1 (en) * 2006-11-30 2009-09-25 Airbus France Sas AIRPLANE WITH REACTORS ARRANGED AT THE BACK
US8616492B2 (en) * 2009-10-09 2013-12-31 Oliver Vtol, Llc Three wing, six tilt-propulsion units, VTOL aircraft
US8708273B2 (en) 2009-10-09 2014-04-29 Oliver Vtol, Llc Three-wing, six tilt-propulsion unit, VTOL aircraft
US8800912B2 (en) * 2009-10-09 2014-08-12 Oliver Vtol, Llc Three wing, six-tilt propulsion unit, VTOL aircraft
US8272594B2 (en) * 2009-10-26 2012-09-25 Aerion Corporation Laminar flow wing optimized for supersonic cruise aircraft
US8448893B2 (en) * 2009-10-26 2013-05-28 Aerion Corporation Laminar flow wing optimized for transonic cruise aircraft
US8783617B2 (en) 2012-04-12 2014-07-22 Lockheed Martin Corporation Aircraft fuselage drag reduction blivet
US9079663B2 (en) 2013-02-27 2015-07-14 Northrop Grumman Systems Corporation Canard-locked oblique wing aircraft
USD764384S1 (en) * 2014-07-15 2016-08-23 Icon Aircraft, Inc. Aircraft delta fin
US10618638B2 (en) * 2015-09-22 2020-04-14 Nctar, Llc Shockwave mitigation system for supersonic aircraft
US9849966B2 (en) 2015-12-18 2017-12-26 The Boeing Company Fuselage structure for accommodating tails and canards of different sizes and shapes
US10427780B2 (en) 2016-10-20 2019-10-01 Bell Helicopter Textron Inc. Electric cold flow tipjet rotorcraft
US10836481B2 (en) * 2017-11-09 2020-11-17 Bell Helicopter Textron Inc. Biplane tiltrotor aircraft
JP7103631B2 (en) * 2018-04-06 2022-07-20 国立研究開発法人宇宙航空研究開発機構 How to reduce supersonic aircraft and sonic booms
CN109305360A (en) * 2018-09-30 2019-02-05 杨清太 Umbellate form jet type helicopters constructive method
CN110186640B (en) * 2019-06-21 2024-04-12 中国商用飞机有限责任公司北京民用飞机技术研究中心 Wing wind tunnel model manufacturing method and wing wind tunnel model
RU194250U1 (en) * 2019-06-27 2019-12-04 Петр Алексеевич Розин Small Elongation Wing for Subsonic Aircraft
CN110341932B (en) * 2019-07-29 2024-07-09 中国科学院力学研究所 High-speed aircraft based on high-pressure capturing wing appearance
CN110406671B (en) * 2019-07-29 2024-07-02 中国科学院力学研究所 Side air inlet high-speed aircraft
CN110341933B (en) * 2019-07-29 2024-06-21 中国科学院力学研究所 Air suction type high-speed aircraft with high-pressure capturing wings
CN113044199B (en) * 2021-04-20 2023-12-15 西北工业大学 High-performance low-Reynolds number serial laminar flow wing profile based on coupling wing layout unmanned aerial vehicle
CN115432171B (en) * 2022-11-07 2023-01-03 中国航空工业集团公司沈阳空气动力研究所 Rear propulsion truss support wing layout suitable for hypersonic transport plane
CN118966090B (en) * 2024-10-21 2024-12-17 中国空气动力研究与发展中心高速空气动力研究所 Airfoil pressure distribution test result densification method

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Also Published As

Publication number Publication date
US20040056150A1 (en) 2004-03-25
WO2002046038A3 (en) 2002-11-07
US6729577B2 (en) 2004-05-04
WO2002046038A2 (en) 2002-06-13
EP1347915A2 (en) 2003-10-01

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