General equations for reduction of flight test climb data to standard air conditions are given, indicating how airplane and engine characteristics affect necessary rate of climb corrections; charts are given to provide aid in reduction of climb data of airplanes having modern engine installations.
Reduction of flight test climb data to standard air conditions
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 7 , n 1 ; p 12-17
1939
6 pages
Bibliography
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
The reduction of flight test data to standard atmosphere conditions
Engineering Index Backfile | 1927
|The reduction of airplane flight test data to standard atmosphere conditions
Engineering Index Backfile | 1925
|