Relationship of swept wing to compressibility and shock wave is shown graphically; reference made to German practice; factors involved in design for Mach Numbers approaching unity and beyond are studied; compromise wing design is suggested.
Swept wing at high velocity
Aeroplane
Aeroplane ; 70 , n 1823 ; p 513-515
1946
3 pages
Aufsatz (Zeitschrift)
Englisch
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