GB402514A - Improved high lift wing section for aeroplanes and the like - Google Patents

Improved high lift wing section for aeroplanes and the like

Info

Publication number
GB402514A
GB402514A GB1859432A GB1859432A GB402514A GB 402514 A GB402514 A GB 402514A GB 1859432 A GB1859432 A GB 1859432A GB 1859432 A GB1859432 A GB 1859432A GB 402514 A GB402514 A GB 402514A
Authority
GB
United Kingdom
Prior art keywords
aeroplanes
lift wing
high lift
wing section
improved high
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
Application number
GB1859432A
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.)
ROBERT GEORGE READ
Original Assignee
ROBERT GEORGE READ
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 ROBERT GEORGE READ filed Critical ROBERT GEORGE READ
Priority to GB1859432A priority Critical patent/GB402514A/en
Publication of GB402514A publication Critical patent/GB402514A/en
Expired legal-status Critical Current

Links

Classifications

    • 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

Abstract

402,514. Aircraft wings. READ, R. G., 25, Croydon Road, Reigate, Surrey. July 1, 1932, No. 18594. [Class 4.] A high-lift wing- section for wings of uniform or tapering construction throughout the span is shaped as shown.
GB1859432A 1932-07-01 1932-07-01 Improved high lift wing section for aeroplanes and the like Expired GB402514A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1859432A GB402514A (en) 1932-07-01 1932-07-01 Improved high lift wing section for aeroplanes and the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1859432A GB402514A (en) 1932-07-01 1932-07-01 Improved high lift wing section for aeroplanes and the like

Publications (1)

Publication Number Publication Date
GB402514A true GB402514A (en) 1933-12-07

Family

ID=10115119

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1859432A Expired GB402514A (en) 1932-07-01 1932-07-01 Improved high lift wing section for aeroplanes and the like

Country Status (1)

Country Link
GB (1) GB402514A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4641796A (en) * 1983-09-30 1987-02-10 The Boeing Company Airfoil
EP1468908A1 (en) * 2003-04-16 2004-10-20 Manuel Munoz Saiz Aerodynamic profile

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4641796A (en) * 1983-09-30 1987-02-10 The Boeing Company Airfoil
EP1468908A1 (en) * 2003-04-16 2004-10-20 Manuel Munoz Saiz Aerodynamic profile

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