Based on comparison between flight measurement results and calculations, data are obtained for sufficiently accurate calculation of resulting normal forces on wing truss structure and horizontal tail surface during accelerated longitudinal motion of elevator controlled airplane.
Flight tests and calculations for determination of atmospheric forces on airplane with elevator action
Flugversuche und Rechnungen zur Bestimmung der Luftkraefte am Flugzeug, etc
1938
Bibliography
Article (Journal)
German
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Determination of airplane critical altitude by flight tests
Engineering Index Backfile | 1942
|Airplane research work through flight tests
Engineering Index Backfile | 1923
British Library Online Contents | 1996
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