A Transonic Wind-tunnel Investigation of the Aerodynamic Characteristics of Three 4-percent-thick Wings of Sweepback Angles 10.8 Degrees, 35 Degrees, and 47 Degrees, Aspect Ratio 3.5, and Taper Ratio 0.2 in Combination with a Body
1952-07-15
Sonstige
Keine Angabe
Englisch