COMPOSITES FOR CIVIL AIRCRAFT.

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Anon

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| 1600年 / 06期

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KEVLAR FIBER;

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[41] SOUND INTENSITY MEASUREMENTS INSIDE AIRCRAFT.
Gade, Svend
S V Sound and Vibration, 1987, 21 (03): : 32 - 36
[42] Mathematical Model of a Subsonic Transport Aircraft.
Latypov, A.F.
Soroka, B.N.
Izvestia Sibirskogo otdelenia Akademii nauk SSSR. Seria tehniceskih nauk, 1981, (13):
[43] AIR CUSHION LANDING SYSTEMS FOR AIRCRAFT.
Goethert, Bernhard H.
1600, DGLR, Cologne, Ger
[44] GEOPHYSICAL SURVEY USING A MICROLIGHT AIRCRAFT.
Lambert, Andre C.
Mining Magazine, 1988, 158 (03): : 194 - 196
[45] HIGH VOLTAGE DESIGN GUIDE: AIRCRAFT.
Dunbar, W.G.
1983, : 82 - 2057
[46] VARIABLE WING CAMBER FOR TRANSPORT AIRCRAFT.
Szodruch, J.
Hilbig, R.
Progress in Aerospace Sciences, 1988, 25 (03) : 297 - 328
[47] UNLOCKING THE POTENTIAL OF METAL MATRIX COMPOSITES FOR CIVIL AIRCRAFT
CHARLES, D
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1991, 135 : 295 - 297
[48] Unlocking the potential of metal matrix composites for civil aircraft
Charles, David
Materials Science and Engineering A, 1991, A135 (1-2) : 295 - 297
[49] DESIGN GUIDE FOR LIGHTNING PROTECTION OF AIRCRAFT.
Plumer, J.Anderson
IEEE International Symposium on Electromagnetic Compatibility, 1979, : 77 - 84
[50] Variables Characterizing the Wind Effects on the Aircraft.
Brockhaus, Rudolf
Zeitschrift fuer Flugwissenschaften und Weltraumforschung, 1979, 3 (04): : 229 - 234