IMPACT OF NEW MATERIALS ON THE DEVELOPMENT OF ROTARY WING AIRCRAFT.

被引：0

作者：

D'Ambra, F.

机构：

来源：

关键词：

Compendex;

D O I：

10.4050/jahs.26.16

中图分类号：

学科分类号：

摘要：

Helicopters, Military

引用

页码：16 / 23

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[1] DEVELOPMENT OF A MISSION ADAPTIVE WING SYSTEM FOR A TACTICAL AIRCRAFT.
Gilbert, Williams W.
AIAA Paper, 1980,
[2] BONDING THE WING OF A BIG AIRCRAFT.
Nelson, Paul K.
Sanders, Willard D.
American machinist, 1982, 126 (12): : 87 - 89
[3] TRANSONIC WING DESIGN FOR TRANSPORT AIRCRAFT.
Krenz, Guenter
Prace Instytutu Metalurgii Zelaza im St. Staszica, 1979, : 52 - 61
[4] COMPUTER PROGRAM FOR PREDICTION OF THE DEPOSITION OF MATERIAL RELEASED FROM FIXED AND ROTARY WING AIRCRAFT.
Teske, Milton E.
NASA Contractor Reports, 1984,
[5] VARIABLE WING CAMBER FOR TRANSPORT AIRCRAFT.
Szodruch, J.
Hilbig, R.
Progress in Aerospace Sciences, 1988, 25 (03) : 297 - 328
[6] ROTARY WING AIRCRAFT
ROBERTS, H
NATURE, 1949, 163 (4132) : 72 - 74
[7] IMPACT OF MICROCLIMATE COOLING IN ROTARY-WING AIRCRAFT
HILL, AJ
AVIATION SPACE AND ENVIRONMENTAL MEDICINE, 1990, 61 (05): : 442 - 442
[8] LOADING TESTS OF A WING STRUCTURE FOR A HYPERSONIC AIRCRAFT.
Fields, Roger A.
Reardon, Lawrence F.
Siegel, William H.
NASA Technical Paper, 1980, (1596):
[9] Rotary-wing aircraft
不详
AVIATION WEEK & SPACE TECHNOLOGY, 2000, 152 (03): : 82 - 91
[10] HIGH-LIFT WING SECTION FOR LIGHT AIRCRAFT.
Marsden, D.J.
Canadian Aeronautics and Space Journal, 1988, 34 (01): : 55 - 61