New method of calculation makes direct use of actual airplane polars without approximations; procedure based on extension of Eiffel-Rith coordinate system, and all scales can be incorporated in simple transparent chart, thereby eliminating necessity for special prepared graph paper; compressibility effects are taken into account through use of constant altitude variable Mach number polars which are derived from constant Mach number polars of true airplane. (See also Aircraft Eng v 16 n 188 Oct 1944 p 281-6, 297)
Logarithmic performance computation
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 11 , n 4
1944
10 pages
Bibliography
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Logarithmic performance computation
Engineering Index Backfile | 1944
|Computation of Unsteady Shock-Induced Combustion Using Logarithmic Species Conservation Equations
Online Contents | 1993
|Airplane performance calculations by means of logarithmic graphs
Engineering Index Backfile | 1938
|