Dynamic-pressure Measurements Using an Electronically Scanned Pressure Module PDF Download
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Author: William G. Chapin
Publisher:
ISBN:
Category : Pressure
Languages : en
Pages : 28
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Book Description
Author: William G. Chapin
Publisher:
ISBN:
Category : Pressure
Languages : en
Pages : 28
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 332
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Author: David A. Seidel
Publisher:
ISBN:
Category :
Languages : en
Pages : 330
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
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Author: Raymond E. Mineck
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 190
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Book Description
A wind tunnel test of a generic helicopter fuselage model with an independently mounted rotor has been conducted to obtain steady and periodic pressure data on the helicopter body. The model was tested at four advance ratios and three thrust coefficients. The periodic unsteady pressure coefficients are marked by four peaks associated with the passage of the four rotor blades. Blade passage effects are largest on the nose and tail boom of the model. The magnitude of the pulse increases with rotor thrust coefficient. Tabular listings of the unsteady pressure data are included to permit independent analysis. A CDrom containing the steady and unsteady pressure data presented in the report is available from the authors.
Author: David M. Schuster
Publisher:
ISBN:
Category : Plates (Engineering)
Languages : en
Pages : 44
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Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 748
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Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 974
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 112
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Author:
Publisher:
ISBN:
Category : Metallurgy
Languages : en
Pages : 1058
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