Range Calculations for Airplanes With Continuously Controllable Pitch Propellers, and the Effect of Certain Geometric Parameters of the Airplane on Range

Range Calculations for Airplanes With Continuously Controllable Pitch Propellers, and the Effect of Certain Geometric Parameters of the Airplane on Range

<p>This investigation was undertaken to develop a satisfactorily exact method for the calculation of range of airplane; and with such method, to determine the effect of certain geometrical parameters of the airplane on range, namely, span, aspect ratio, and wing loading.</p> <p>...

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Bibliographic Details
Main Authors: Scoles, Albert Buddy, Schoech, William Alton
Format: Others
Published: 1938
Online Access:https://thesis.library.caltech.edu/547/1/Scoles_ab_1938.pdf
Scoles, Albert Buddy and Schoech, William Alton (1938) Range Calculations for Airplanes With Continuously Controllable Pitch Propellers, and the Effect of Certain Geometric Parameters of the Airplane on Range. Master's thesis, California Institute of Technology. doi:10.7907/CMHQ-E314. https://resolver.caltech.edu/CaltechETD:etd-02082006-090132 <https://resolver.caltech.edu/CaltechETD:etd-02082006-090132>

Internet

https://thesis.library.caltech.edu/547/1/Scoles_ab_1938.pdf
Scoles, Albert Buddy and Schoech, William Alton (1938) Range Calculations for Airplanes With Continuously Controllable Pitch Propellers, and the Effect of Certain Geometric Parameters of the Airplane on Range. Master's thesis, California Institute of Technology. doi:10.7907/CMHQ-E314. https://resolver.caltech.edu/CaltechETD:etd-02082006-090132 <https://resolver.caltech.edu/CaltechETD:etd-02082006-090132>

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