Experimental Investigation of the Effects of Aft Blowing with Various Nozzle Exit Geometries on a 3.0 Caliber Tangent Ogive at High Angles of Attack: Forebody Pressure Distributions
Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781722387938


Pages:   98
Publication Date:   06 July 2018
Format:   Paperback
Availability:   Available To Order   Availability explained
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Experimental Investigation of the Effects of Aft Blowing with Various Nozzle Exit Geometries on a 3.0 Caliber Tangent Ogive at High Angles of Attack: Forebody Pressure Distributions


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Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
Imprint:   Createspace Independent Publishing Platform
Dimensions:   Width: 21.60cm , Height: 0.50cm , Length: 27.90cm
Weight:   0.249kg
ISBN:  

9781722387938


ISBN 10:   1722387939
Pages:   98
Publication Date:   06 July 2018
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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