Review of two lectures presented at Training Center for Experimental Aerodynamics at Rhode Saint-Genese, Brussels, Jan 21 and 22; area rule may be applied up to Mach number of 2.0; most important theoretical application is that, by use of area rule, equivalent axially symmetrical bodies can be found, amenable to theoretical calculations for drag; practical application. See also Engineering Index 1956 p 38, under Aircraft Design -- Drag.
Scope of area-rule
Aeroplane
Aeroplane ; 94 , n 2422
1958
2 pages
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1956
Engineering Index Backfile | 1955
Engineering Index Backfile | 1955
NTIS | 1977
|AIAA | 1963
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