Scale-effect Tests in a Turbulent Tunnel of the NACA 653-418, a = 1.0 Airfoil Section With 0.20-airfoil-chord Split Flap
Product ID: 1014267110
Condition: New
$ 73
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Product Description
Scale-effect Tests in a Turbulent Tunnel of the NACA 653-418, a = 1.0 Airfoil Section With 0.20-airfoil-chord Split Flap
Technical Specifications
Country
USA
Manufacturer
Hassell Street Press
Binding
Paperback
PartNumber
RKC2012246631
Height
9.21
Length
6.14
Weight
0.14109584768
Width
0.07
NumberOfItems
1







