FR957054A - - Google Patents

Info

Publication number
FR957054A
FR957054A FR957054DA FR957054A FR 957054 A FR957054 A FR 957054A FR 957054D A FR957054D A FR 957054DA FR 957054 A FR957054 A FR 957054A
Authority
FR
France
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
Application number
Other languages
French (fr)
Publication date
Application granted granted Critical
Publication of FR957054A publication Critical patent/FR957054A/fr
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/54Varying in area
    • B64C3/546Varying in area by foldable elements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/54Varying in area

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR957054D Expired FR957054A (en)

Publications (1)

Publication Number Publication Date
FR957054A true FR957054A (en) 1950-02-14

Family

ID=1559439

Family Applications (1)

Application Number Title Priority Date Filing Date
FR957054D Expired FR957054A (en)

Country Status (1)

Country Link
FR (1) FR957054A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4235400A (en) * 1979-05-10 1980-11-25 Juanita June Haworth Hi-lo two speed wing
US4962903A (en) * 1987-10-19 1990-10-16 Red Eye Arms, Inc. Cooling method and apparatus for wings and other fuselage components
US6464171B2 (en) * 1997-04-04 2002-10-15 Georgia Tech Research Corp. Leading edge channel for enhancement of lift/drag ratio and reduction of sonic boom
WO2003039949A2 (en) * 2001-10-18 2003-05-15 Dragutin Bosatlic Wing with lift enhancement by internal air flow
CN104097765A (en) * 2014-08-03 2014-10-15 佛山市神风航空科技有限公司 Dual-layer flat airfoil

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4235400A (en) * 1979-05-10 1980-11-25 Juanita June Haworth Hi-lo two speed wing
US4962903A (en) * 1987-10-19 1990-10-16 Red Eye Arms, Inc. Cooling method and apparatus for wings and other fuselage components
US6464171B2 (en) * 1997-04-04 2002-10-15 Georgia Tech Research Corp. Leading edge channel for enhancement of lift/drag ratio and reduction of sonic boom
WO2003039949A2 (en) * 2001-10-18 2003-05-15 Dragutin Bosatlic Wing with lift enhancement by internal air flow
WO2003039949A3 (en) * 2001-10-18 2004-08-12 Dragutin Bosatlic Wing with lift enhancement by internal air flow
CN104097765A (en) * 2014-08-03 2014-10-15 佛山市神风航空科技有限公司 Dual-layer flat airfoil

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