Sayap kanal: Perbedaan antara revisi
Tampilan
Konten dihapus Konten ditambahkan
k ArdWar memindahkan halaman Channel wing ke Sayap kanal |
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[[Kategori:Konfigurasi sayap pesawat terbang]] |
[[Kategori:Konfigurasi sayap pesawat terbang]] |
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[[Kategori:Desain sayap pesawat terbang]] |
[[Kategori:Desain sayap pesawat terbang]] |
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[[Kategori:Pesawat terbang sayap kanal]] |
Revisi per 23 Mei 2014 15.24
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, kemudi baling-baling ditempatkan di ujung belakang saluran dibentuk oleh setengah tabung.
Referensi
- 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-1 National Air and Space Museum[pranala nonaktif]
- Pictures of the Custer CCW-5 Mid-Atlantic Air Museum, Reading, Pennsylvania
- Modern channelwing aircraft design Stavatti designed channelwing transport for the 2000s