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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
Other languages
English (en)
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

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C30/00Supersonic type aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/06Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B64C39/068Aircraft not otherwise provided for having disc- or ring-shaped wings having multiple wings joined at the tips
    • 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)
  • 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 (fr) 2000-12-08 2001-12-06 Avion a voilure haubanee a la queue et configurations d'un avion long-courrier supersonique a faible bang sonique

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 (fr)
EP (1) EP1347915A2 (fr)
AU (1) AU2002227282A1 (fr)
WO (1) WO2002046038A2 (fr)

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US20060157613A1 (en) * 2005-01-19 2006-07-20 Adamson Eric E Supersonic aircraft with active lift distribution control for reducing sonic boom
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US7410122B2 (en) * 2006-03-20 2008-08-12 The Boeing Company VTOL UAV with lift fans in joined wings
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US7946535B2 (en) * 2006-10-18 2011-05-24 Aerion Corporation Highly efficient supersonic laminar flow wing
US20080114575A1 (en) * 2006-10-24 2008-05-15 The Boeing Company Systems and methods for performing load analysis
US20080105783A1 (en) * 2006-11-03 2008-05-08 Cessna Aircraft Company Fuselage design for sonic boom suppression of supersonic aircraft
FR2908107B1 (fr) * 2006-11-06 2008-12-19 Airbus France Sa Procede et dispositif pour estimer les forces s'exercant sur une surface de controle d'un aeronef.
FR2909359B1 (fr) * 2006-11-30 2009-09-25 Airbus France Sas Avion a reacteurs disposes a l'arriere
US8616492B2 (en) * 2009-10-09 2013-12-31 Oliver Vtol, Llc Three wing, six tilt-propulsion units, VTOL aircraft
US8800912B2 (en) 2009-10-09 2014-08-12 Oliver Vtol, Llc Three wing, six-tilt propulsion unit, VTOL aircraft
US8708273B2 (en) 2009-10-09 2014-04-29 Oliver Vtol, Llc Three-wing, six tilt-propulsion unit, VTOL aircraft
US8448893B2 (en) * 2009-10-26 2013-05-28 Aerion Corporation Laminar flow wing optimized for transonic cruise aircraft
US8272594B2 (en) * 2009-10-26 2012-09-25 Aerion Corporation Laminar flow wing optimized for supersonic 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 (ja) * 2018-04-06 2022-07-20 国立研究開発法人宇宙航空研究開発機構 超音速機及びソニックブームの低減方法
CN109305360A (zh) * 2018-09-30 2019-02-05 杨清太 伞型喷气式直升飞机构成方法
CN110186640B (zh) * 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 一种机翼风洞模型制造方法及机翼风洞模型
RU194250U1 (ru) * 2019-06-27 2019-12-04 Петр Алексеевич Розин Крыло малого удлинения для дозвукового летательного аппарата
CN110406671B (zh) * 2019-07-29 2024-07-02 中国科学院力学研究所 一种旁侧进气高速飞行器
CN110341932B (zh) * 2019-07-29 2024-07-09 中国科学院力学研究所 一种基于高压捕获翼外形的高速飞行器
CN110341933B (zh) * 2019-07-29 2024-06-21 中国科学院力学研究所 一种具有高压捕获翼的吸气式高速飞行器
CN113044199B (zh) * 2021-04-20 2023-12-15 西北工业大学 基于联结翼布局无人机的高性能低雷诺数串置层流翼型
CN115432171B (zh) * 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 一种适用于高亚声速运输机的后置推进桁架支撑机翼布局
CN115848621A (zh) * 2022-12-22 2023-03-28 中国航空工业集团公司西安飞机设计研究所 一种军用运输机
CN118966090B (zh) * 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 一种翼型压力分布试验结果增密方法

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Also Published As

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

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