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Terminal Nose‐Dives: Two Articles on the Calculation of Speeds Attained and Stresses Incurred

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 May 1941

Abstract

DURING a nose‐dive from a height H0 at a constant angle of inclination of the flight path, the equation of forces in the direction of flight is

Citation

Groth, E. and Scheubel, F.N. (1941), "Terminal Nose‐Dives: Two Articles on the Calculation of Speeds Attained and Stresses Incurred", Aircraft Engineering and Aerospace Technology, Vol. 13 No. 5, pp. 120-122. https://doi.org/10.1108/eb030766

Publisher

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MCB UP Ltd

Copyright © 1941, MCB UP Limited