Theoretical Analysis of Aerodynamic Characteristics of Two Helicopter Rotor Airfoils
Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781724747082


Pages:   32
Publication Date:   06 August 2018
Format:   Paperback
Availability:   Available To Order   Availability explained
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Theoretical Analysis of Aerodynamic Characteristics of Two Helicopter Rotor Airfoils


Overview

An analytical study was conducted to predict the aerodynamic characteristics of two helicopter rotor airfoils. Documentation of the predictive process covers the development of empirical factors used in conjunction with computer programs for airfoil analysis. Tables of lift, drag, and pitching-moment coefficient for each airfoil were prepared for two dimensional, steady flow conditions at Mach numbers from 0.3 to 0.9 and Reynolds numbers of 7,700,000 to 23,000,000, respectively. Morris, C. E. K., Jr. and Yeager, W. T., Jr. Langley Research Center NASA-TM-78680 RTOP 505-10-23-07

Full Product Details

Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
Imprint:   Createspace Independent Publishing Platform
Dimensions:   Width: 21.60cm , Height: 0.20cm , Length: 28.00cm
Weight:   0.102kg
ISBN:  

9781724747082


ISBN 10:   1724747088
Pages:   32
Publication Date:   06 August 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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