Sayap kanal

Channelwing aircraft

^[1]Sayap Channel adalah prinsip sayap pesawat yang dikembangkan oleh Willard Ray Custer pada tahun 1920. Bagian paling penting dari sayap terdiri dari setengah tabung dengan mesin ditempatkan di tengah. Bagian kemudi baling-baling ditempatkan di ujung belakang saluran dibentuk oleh setengah tabung.https://www.youtube.com/watch?v=7FhFlxbV-AU^[2] http://www.angelfire.com/va3/bythefire/

Referensi

^ "Welcome to the Custer Channelwing Website". web.archive.org. 2010-02-15. Archived from the original on 2010-02-15. Diakses tanggal 2021-07-30. Pemeliharaan CS1: Url tak layak (link)
^ Eldred, Wendell E. (1953-01-01). "LANDING GEAR DESIGN AS APPLIED TO MODERN AIRCRAFT". SAE Technical Paper Series. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International. doi:10.4271/530157.

Donald Liska - Channelwing aircraft, The Wisconsin engineer Vol. 57, Nr. 6, pp 16 –19, October 1957, [1]
Kevin Brown - Cockpit-Testing the Legendary Channel-Wing, Popular Mechanics, September 1964
Robert Englar, Brian Campbell - Development of Pneumatic Channel Wing Powered-Lift Advanced Super-STOL Aircraft, 1st Flow Control Conference 24–26 June 2002, AIAA 2002-3275, St. Luis, Missouri, 2002
Walt Boyne - The Custer Channel Wing Story, Airpower Magazine, Volume 7 No.3 May 1977
Unknown author - Custer's Production Model Takes Bow, Air Progress Magazine, October/November, 1964
Unknown author - Channel Wing Flown in Demonstration, Aviation Week, September 28, 1959

Pranala luar

Custer-Channelwing Website Archive
Another Custer Channel Wing Website
Video of Custer explaining his theories and actual flight footage
Pictures of the Custer CCW-1National Air and Space Museum Diarsipkan 2007-06-10 di Wayback Machine.
Pictures of the Custer CCW-5 Mid-Atlantic Air Museum, Reading, Pennsylvania
Modern channelwing aircraft design Diarsipkan 2008-02-02 di Wayback Machine. Stavatti designed channelwing transport for the 2000s

Komponen dan sistem pesawat terbang

Kerangka