Scale-effect Tests in a Turbulent Tunnel of the NACA 653-418, a = 1.0 Airfoil Section With 0.20-airfoil-chord Split Flap
Author:   Langley Aeronautical Laboratory
Publisher:   Hassell Street Press
ISBN:  

9781014267115


Pages:   34
Publication Date:   09 September 2021
Format:   Paperback
Availability:   Available To Order   Availability explained
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Scale-effect Tests in a Turbulent Tunnel of the NACA 653-418, a = 1.0 Airfoil Section With 0.20-airfoil-chord Split Flap


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Author:   Langley Aeronautical Laboratory
Publisher:   Hassell Street Press
Imprint:   Hassell Street Press
Dimensions:   Width: 15.60cm , Height: 0.20cm , Length: 23.40cm
Weight:   0.064kg
ISBN:  

9781014267115


ISBN 10:   1014267110
Pages:   34
Publication Date:   09 September 2021
Audience:   General/trade ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   Available To Order   Availability explained
We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately.

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