Performance of B. M. W. 185-horsepower airplane engine
Description:
Report discusses the results of testing on a B.M.W. engine in an altitude chamber where temperature and pressure can be controlled to simulate flight at various altitudes. Results for various engine speeds, altitudes, and propeller speeds are provided.
Date:
April 13, 1922
Creator:
Sparrow, Stanwood Willston
Partner:
UNT Libraries Government Documents Department