Advantages over other types of structure; adaptability to machine manufacture for production and design considerations to best accomplish normal life of structure which may be expected under continued service; and frequency of overhaul necessary to basic structure during life of airplane.
Stressed-skin structures for aircraft
Soc Automotive Engrs -- J
Society of Automotive Engineers -- Journal ; 39 , n 5
1936
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Stressed-Skin Structures for Aircraft
SAE Technical Papers | 1936
|Engineering Index Backfile | 1935
|Engineering Index Backfile | 1935
|Emerald Group Publishing | 1935
|Dornier Stressed-Skin Structures
Emerald Group Publishing | 1939
|