DE60300441D1 - Hinterkante eines Tragflächenprofils mit laminarer Strömung - Google Patents
Hinterkante eines Tragflächenprofils mit laminarer StrömungInfo
- Publication number
- DE60300441D1 DE60300441D1 DE60300441T DE60300441T DE60300441D1 DE 60300441 D1 DE60300441 D1 DE 60300441D1 DE 60300441 T DE60300441 T DE 60300441T DE 60300441 T DE60300441 T DE 60300441T DE 60300441 D1 DE60300441 D1 DE 60300441D1
- Authority
- DE
- Germany
- Prior art keywords
- trailing edge
- laminar flow
- wing profile
- flow wing
- profile
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/14—Aerofoil profile
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/14—Aerofoil profile
- B64C2003/149—Aerofoil profile for supercritical or transonic flow
-
- 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)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2002170786A JP4237980B2 (ja) | 2002-06-12 | 2002-06-12 | 飛行機の主翼用層流翼型 |
| JP2002170786 | 2002-06-12 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE60300441D1 true DE60300441D1 (de) | 2005-05-04 |
| DE60300441T2 DE60300441T2 (de) | 2006-02-09 |
Family
ID=29561766
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE60300441T Expired - Lifetime DE60300441T2 (de) | 2002-06-12 | 2003-02-26 | Hinterkante eines Tragflächenprofils mit laminarer Strömung |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7093792B2 (de) |
| EP (1) | EP1371550B1 (de) |
| JP (1) | JP4237980B2 (de) |
| DE (1) | DE60300441T2 (de) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7850126B2 (en) * | 2007-04-25 | 2010-12-14 | The Boeing Company | Laminar flow surfaces with selected roughness distributions, and associated methods |
| US7866609B2 (en) * | 2007-06-15 | 2011-01-11 | The Boeing Company | Passive removal of suction air for laminar flow control, and associated systems and methods |
| JP5067104B2 (ja) * | 2007-10-03 | 2012-11-07 | トヨタ自動車株式会社 | 車両下部構造 |
| CN101492090B (zh) * | 2008-01-22 | 2012-08-29 | 西北工业大学 | 一种后缘分离涡高升力高速层流翼型 |
| RU2406647C1 (ru) * | 2009-06-15 | 2010-12-20 | Закрытое акционерное общество "Гражданские самолеты Сухого" | Стреловидное крыло самолета и аэродинамический профиль (варианты) |
| US8448893B2 (en) * | 2009-10-26 | 2013-05-28 | Aerion Corporation | Laminar flow wing optimized for transonic cruise aircraft |
| WO2012060230A1 (ja) * | 2010-11-02 | 2012-05-10 | 独立行政法人宇宙航空研究開発機構 | 超音速飛翔体用機首 |
| US9868525B2 (en) * | 2015-09-25 | 2018-01-16 | The Boeing Company | Low speed airfoil design for aerodynamic improved performance of UAVs |
| RU2645557C1 (ru) * | 2016-11-17 | 2018-02-21 | Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") | Крыло летательного аппарата |
| EP3363733B1 (de) | 2017-02-18 | 2021-11-10 | Jean-Eloi William Lombard | Passivströmungsteuerungsmechanismus zur abschwächung und/oder unterdrückung von tollmien-schlichting-wellen, zur verzögerung des übergangs zu turbulenzen und zur verringerung des widerstands |
| CN110498037B (zh) * | 2019-08-22 | 2020-09-08 | 西安探索鹰航空科技有限公司 | 一种适用于低空低速无人机的高升阻比层流翼型 |
| CN111498084A (zh) * | 2020-04-15 | 2020-08-07 | 成都飞机工业(集团)有限责任公司 | 一种应用于高空高速长航时无人机的低阻层流翼型 |
| CN112572761B (zh) * | 2020-12-14 | 2022-09-09 | 西北工业大学 | 一种具有低阻高发散马赫数高升力的跨空域稳健层流翼型 |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB615318A (en) * | 1944-06-07 | 1949-01-05 | Glenn L Martin Co | Improvements in or relating to low drag airfoils |
| US3952971A (en) * | 1971-11-09 | 1976-04-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Airfoil shape for flight at subsonic speeds |
| GB1554713A (en) * | 1975-03-04 | 1979-10-24 | Secr Defence | Wings |
| DE2712717A1 (de) * | 1977-03-23 | 1978-09-28 | Ver Flugtechnische Werke | Ueberkritisches tragfluegelprofil |
| FR2427249A1 (fr) * | 1978-05-29 | 1979-12-28 | Aerospatiale | Profil de voilure pour aeronef |
| FR2490586A1 (fr) * | 1980-09-24 | 1982-03-26 | Aerospatiale | Profil de pale pour voilure tournante d'aeronef |
| DE3140351C2 (de) * | 1981-10-10 | 1987-02-12 | Dornier Gmbh, 7990 Friedrichshafen | Profile, insbesondere Tragflügelprofile für Luftfahrzeuge |
| US4718619A (en) * | 1983-07-28 | 1988-01-12 | Ministry Of Defence | Manoeuverable supercritical wing section |
| US4776531A (en) * | 1986-09-05 | 1988-10-11 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | High lift, low pitching moment airfoils |
| US4858852A (en) * | 1987-06-01 | 1989-08-22 | Mcdonnell Douglas Corporation | Divergent trailing-edge airfoil |
| JP2633413B2 (ja) * | 1991-06-03 | 1997-07-23 | 富士重工業株式会社 | 回転翼航空機の回転翼羽根 |
| US5318249A (en) * | 1992-04-14 | 1994-06-07 | The Boeing Company | Curled trailing edge airfoil |
| GB9828447D0 (en) * | 1998-12-24 | 1999-02-17 | Secr Defence Brit | Wing trailing edge |
-
2002
- 2002-06-12 JP JP2002170786A patent/JP4237980B2/ja not_active Expired - Lifetime
-
2003
- 2003-02-26 EP EP03004177A patent/EP1371550B1/de not_active Expired - Lifetime
- 2003-02-26 DE DE60300441T patent/DE60300441T2/de not_active Expired - Lifetime
- 2003-02-27 US US10/373,694 patent/US7093792B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| US7093792B2 (en) | 2006-08-22 |
| JP4237980B2 (ja) | 2009-03-11 |
| JP2004010020A (ja) | 2004-01-15 |
| US20030230669A1 (en) | 2003-12-18 |
| EP1371550B1 (de) | 2005-03-30 |
| DE60300441T2 (de) | 2006-02-09 |
| EP1371550A1 (de) | 2003-12-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8364 | No opposition during term of opposition |