Love, E. S. (1955). Investigations at supersonic speeds of 22 triangular wings representing twoairfoil sections for each of 11 apex angles. NACA.
Chicago-Zitierstil (17. Ausg.)Love, Eugene S. Investigations at Supersonic Speeds of 22 Triangular Wings Representing Twoairfoil Sections for Each of 11 Apex Angles. Washington: NACA, 1955.
MLA-Zitierstil (9. Ausg.)Love, Eugene S. Investigations at Supersonic Speeds of 22 Triangular Wings Representing Twoairfoil Sections for Each of 11 Apex Angles. NACA, 1955.
Achtung: Diese Zitate sind unter Umständen nicht zu 100% korrekt.