DocumentCode :
20083
Title :
Investigation at low speed of a six-percent thick symmetrical circular-arc airfoil with leading edge retraction in combination with nose slot
University :
Cahech Library System
Grade :
نامعلوم
Major :
Engineers Degree )Aeronautic(
Number of pages :
0
Publish Date :
1955
Note :
01
Language :
انگليسي
Link To Document :
https://search.ricest.ac.ir/dl/search/defaultta.aspx?DTC=17&DC=20083