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 J Aeronautical Sciences v 11 n 4 Oct 1944 p 329-38)
Logarithmic performance computation
Aircraft Eng
Aircraft Engineering ; 16 , n 188
1944
Bibliography
Aufsatz (Zeitschrift)
Englisch
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Logarithmic performance computation
Engineering Index Backfile | 1944
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Online Contents | 1993
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