Pengaruh Buckling Terhadap Kestabilan Pesawat Terbang  

Oleh:

Soediro, Y.B. Moelyanto

Jenis: Article from Journal - ilmiah nasional - tidak terakreditasi DIKTI - atma jaya
Dalam koleksi: Atma nan Jaya vol. 18 no. 3 (Dec. 2003), page 49-60.
Topik: ELASTICITY; modulus of elasticity; crippling stress; flexural instability
Fulltext: Y.B. Moelyanto Soediro.pdf (495.41KB)

Ketersediaan

Perpustakaan Pusat (Semanggi) Nomor Panggil: AA48.13 Non-tandon: 1 (dapat dipinjam: 0) Tandon: tidak ada	Lihat Detail Induk
Perpustakaan PKPM Nomor Panggil: A66 Non-tandon: 1 (dapat dipinjam: 0) Tandon: tidak ada	Lihat Detail Induk

Isi artikel

The most important structural components of an aircraft, namely, the wings fuselage and empenage, are considered from the point of view of stressing as beams or cantilevers with variable loading along their lengths. The primary structure of an airplane usually consists basically of a box beam. The main structural consists box of wing tail plane is a well-known example, a semi monocoque fusekage is another. For any given loading condition of the aircraft, the material in the box is stressed mainly in tension, in shear, or in compression, depending on its location in the box cross-section, The trend of modern design has been towards the thick stiffened skin type of construction, the thick skin being needed for torsional stiffness in the case of the wings or tail planes and for carrying pressuring loads in the case of fuselage.

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