SE7703463L - Flygvingeform for flygning vid underljudshastigheter - Google Patents

Flygvingeform for flygning vid underljudshastigheter

Info

Publication number
SE7703463L
SE7703463L SE7703463A SE7703463A SE7703463L SE 7703463 L SE7703463 L SE 7703463L SE 7703463 A SE7703463 A SE 7703463A SE 7703463 A SE7703463 A SE 7703463A SE 7703463 L SE7703463 L SE 7703463L
Authority
SE
Sweden
Prior art keywords
flying
sound speeds
wing form
airfoil
trailing edge
Prior art date
Application number
SE7703463A
Other languages
English (en)
Swedish (sv)
Inventor
R T Whitcomb
Original Assignee
Nasa
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 Nasa filed Critical Nasa
Publication of SE7703463L publication Critical patent/SE7703463L/xx

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/04Influencing air flow over aircraft surfaces, not otherwise provided for by generating shock waves
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/10Shape of wings
    • B64C3/14Aerofoil profile
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/10Shape of wings
    • B64C3/14Aerofoil profile
    • B64C2003/142Aerofoil profile with variable camber along the airfoil chord
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/10Shape of wings
    • B64C3/14Aerofoil profile
    • B64C2003/149Aerofoil profile for supercritical or transonic 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)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
SE7703463A 1971-11-09 1977-03-25 Flygvingeform for flygning vid underljudshastigheter SE7703463L (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/197,183 US3952971A (en) 1971-11-09 1971-11-09 Airfoil shape for flight at subsonic speeds

Publications (1)

Publication Number Publication Date
SE7703463L true SE7703463L (sv) 1977-03-25

Family

ID=22728383

Family Applications (2)

Application Number Title Priority Date Filing Date
SE7214434A SE395427B (sv) 1971-11-09 1972-11-08 Flygvinge avsedd spec for ett nachtal mellan 0,7 och 1,0
SE7703463A SE7703463L (sv) 1971-11-09 1977-03-25 Flygvingeform for flygning vid underljudshastigheter

Family Applications Before (1)

Application Number Title Priority Date Filing Date
SE7214434A SE395427B (sv) 1971-11-09 1972-11-08 Flygvinge avsedd spec for ett nachtal mellan 0,7 och 1,0

Country Status (11)

Country Link
US (1) US3952971A (xx)
JP (1) JPS4858599A (xx)
AU (1) AU474789B2 (xx)
CA (1) CA953699A (xx)
DE (1) DE2254888C2 (xx)
FR (1) FR2159422B1 (xx)
GB (1) GB1406826A (xx)
IL (1) IL40766A (xx)
IT (1) IT975491B (xx)
NL (1) NL165423B (xx)
SE (2) SE395427B (xx)

Families Citing this family (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1554713A (en) * 1975-03-04 1979-10-24 Secr Defence Wings
GB1553816A (en) * 1975-06-12 1979-10-10 Secr Defence Wings
DE2712717A1 (de) * 1977-03-23 1978-09-28 Ver Flugtechnische Werke Ueberkritisches tragfluegelprofil
US4142837A (en) * 1977-11-11 1979-03-06 United Technologies Corporation Helicopter blade
FR2427249A1 (fr) * 1978-05-29 1979-12-28 Aerospatiale Profil de voilure pour aeronef
US4311289A (en) * 1978-09-11 1982-01-19 The Dee Howard Company Modifications to jet aircraft having aft fuselage-mounted nacelles overlapping the wing assemblies
FR2463054A1 (fr) * 1979-08-10 1981-02-20 Aerospatiale Profil de pale pour voilure tournante d'aeronef
FR2485470A2 (fr) * 1980-06-30 1981-12-31 Aerospatiale Profil de pale pour voilure tournante d'aeronef
CA1141738A (fr) * 1979-08-10 1983-02-22 Jacques Gallot Profil de pale voilure tournante d'aeronef
GB2072600B (en) * 1980-03-13 1983-11-09 Secr Defence Supercritical aerofoil section
US4431376A (en) * 1980-10-27 1984-02-14 United Technologies Corporation Airfoil shape for arrays of airfoils
DE3208970A1 (de) * 1981-07-01 1983-01-20 Dornier Gmbh, 7990 Friedrichshafen Tragfluegel fuer flugzeuge mit kurzstart- und kurzlandeeigenschaften
US4519746A (en) * 1981-07-24 1985-05-28 United Technologies Corporation Airfoil blade
DE3140351A1 (de) * 1981-10-10 1983-04-28 Dornier Gmbh, 7990 Friedrichshafen "profile, insbesondere tragfluegelprofile fuer luftfahrzeuge"
DE3140350A1 (de) * 1981-10-10 1983-04-28 Dornier Gmbh, 7990 Friedrichshafen Profile, insbesondere tragfluegelprofile fuer luftfahrzeuge
EP0103478A1 (en) * 1982-09-13 1984-03-21 Ian James Gilchrist Airfoil
AU555526B2 (en) * 1982-10-29 1986-09-25 General Electric Company Aircraft engine nacelle
US4799633A (en) * 1982-10-29 1989-01-24 General Electric Company Laminar flow necelle
JPS59100088A (ja) * 1982-11-30 1984-06-09 Sanshin Ind Co Ltd 船舶推進機用プロペラ
US4718619A (en) * 1983-07-28 1988-01-12 Ministry Of Defence Manoeuverable supercritical wing section
US4641796A (en) * 1983-09-30 1987-02-10 The Boeing Company Airfoil
WO1985003051A1 (en) * 1984-01-16 1985-07-18 The Boeing Company An airfoil having improved lift capability
AU598498B2 (en) * 1986-12-12 1990-06-28 Robert B. Wheat High drag airfoil apparatus
US4858852A (en) * 1987-06-01 1989-08-22 Mcdonnell Douglas Corporation Divergent trailing-edge airfoil
US4834617A (en) * 1987-09-03 1989-05-30 United Technologies Corporation Airfoiled blade
US4941803A (en) * 1989-02-01 1990-07-17 United Technologies Corporation Airfoiled blade
US5897076A (en) * 1991-07-08 1999-04-27 Tracy; Richard R. High-efficiency, supersonic aircraft
US6149101A (en) * 1991-07-08 2000-11-21 Tracy; Richard R. Aircraft wing and fuselage contours
US5318249A (en) * 1992-04-14 1994-06-07 The Boeing Company Curled trailing edge airfoil
US5342004A (en) * 1992-10-02 1994-08-30 Eagle Aerospace, Inc. Airfoil trailing flap
GB9828447D0 (en) 1998-12-24 1999-02-17 Secr Defence Brit Wing trailing edge
JP4237980B2 (ja) * 2002-06-12 2009-03-11 本田技研工業株式会社 飛行機の主翼用層流翼型
GB0223249D0 (en) * 2002-10-08 2002-11-13 Amersham Plc Improved imaging agents
WO2006066140A2 (en) * 2004-12-17 2006-06-22 Mead Kirby J Low-drag fin and foil system for surfboards
AU2012219417B2 (en) * 2004-12-17 2016-01-14 Kirby J. Mead Low-drag fin and foil system for surfboards
US8328593B2 (en) 2004-12-17 2012-12-11 Kirby J Mead Low-drag fin and foil system for surfboards
US8186616B2 (en) * 2004-12-21 2012-05-29 Israel Aerospace Industries Ltd. Hybrid transonic-subsonic aerofoils
US7685713B2 (en) * 2005-08-09 2010-03-30 Honeywell International Inc. Process to minimize turbine airfoil downstream shock induced flowfield disturbance
DE102008052858B9 (de) 2008-10-23 2014-06-12 Senvion Se Profil eines Rotorblatts und Rotorblatt einer Windenergieanlage
GB2506357B (en) * 2012-09-26 2015-01-28 Rolls Royce Plc Machining of an article
CN103818545B (zh) * 2012-11-16 2016-04-20 哈尔滨飞机工业集团有限责任公司 一种高升阻比的亚音速翼型
JP5825339B2 (ja) * 2013-12-27 2015-12-02 ダイキン工業株式会社 クロスフローファンの翼
US9709026B2 (en) * 2013-12-31 2017-07-18 X Development Llc Airfoil for a flying wind turbine
CN104176234B (zh) * 2014-08-19 2016-03-02 西北工业大学 一种具有高升阻比滑翔特性的仿翼龙翼型
US10850827B2 (en) * 2014-08-21 2020-12-01 Juan Gerardo Narvaez Tijerina Airfoils for stunt flights
RU2685372C2 (ru) * 2014-08-21 2019-04-17 ТИХЕРИНА Хуан Херардо НАРВАЭС Аэродинамический профиль (варианты) и крыло
CN104691739B (zh) * 2015-03-11 2016-09-14 西北工业大学 一种低阻高阻力发散马赫数的高升力层流翼型
US9868525B2 (en) 2015-09-25 2018-01-16 The Boeing Company Low speed airfoil design for aerodynamic improved performance of UAVs
US10815010B2 (en) 2017-12-27 2020-10-27 Intercept Nexus, Llc High altitude air launched rocket
GB2595724B (en) * 2020-06-05 2022-10-05 Rolls Royce Plc Nacelle for gas turbine engine and aircraft comprising the same
CN114987735B (zh) * 2022-08-08 2022-12-30 中国空气动力研究与发展中心计算空气动力研究所 宽速域低声爆低阻翼型的确定方法和状态构型

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1889864A (en) * 1929-09-06 1932-12-06 Merrill Aircraft Company Airplane
US2833492A (en) * 1955-02-07 1958-05-06 Harlan D Fowler Boundary layer control system with aerodynamic glove

Also Published As

Publication number Publication date
AU474789B2 (en) 1976-08-05
IL40766A0 (en) 1973-01-30
JPS4858599A (xx) 1973-08-16
CA953699A (en) 1974-08-27
SE395427B (sv) 1977-08-15
GB1406826A (en) 1975-09-17
FR2159422A1 (xx) 1973-06-22
IL40766A (en) 1975-06-25
DE2254888C2 (de) 1984-04-12
AU4870172A (en) 1974-05-09
NL7215161A (xx) 1973-05-11
NL165423B (nl) 1980-11-17
FR2159422B1 (xx) 1977-07-29
DE2254888A1 (de) 1973-05-10
US3952971A (en) 1976-04-27
IT975491B (it) 1974-07-20

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