Wind tunnel investigation of a supersonic tailless airplane at low subsonic speed

Wind tunnel investigation of a supersonic tailless airplane at low subsonic speed

An investigation was made in the Cal Tech-Merrill low speed wind tunnel at Pasadena City College to determine the lift and moment characteristics of a sweptback wing and a comparable delta wing, both with a 65° sweptback leading edge and a double wedge symmetrical airfoil section. Both wings were te...

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Bibliographic Details
Main Author: Jensen, Arnold A.
Format: Others
Published: 1948
Online Access:https://thesis.library.caltech.edu/5076/1/Jensen_aa_1948.pdf
Jensen, Arnold A. (1948) Wind tunnel investigation of a supersonic tailless airplane at low subsonic speed. Engineer's thesis, California Institute of Technology. doi:10.7907/KFRK-AF65. https://resolver.caltech.edu/CaltechETD:etd-12192008-103750 <https://resolver.caltech.edu/CaltechETD:etd-12192008-103750>

Internet

https://thesis.library.caltech.edu/5076/1/Jensen_aa_1948.pdf
Jensen, Arnold A. (1948) Wind tunnel investigation of a supersonic tailless airplane at low subsonic speed. Engineer's thesis, California Institute of Technology. doi:10.7907/KFRK-AF65. https://resolver.caltech.edu/CaltechETD:etd-12192008-103750 <https://resolver.caltech.edu/CaltechETD:etd-12192008-103750>

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