NASA NACA-TN-4405-1958 当马赫数在0.75至1.35之间时,测定带有或不带有跨音速压痕抛物线机身的平坦和V字形挡风玻璃遮篷阻力的自由飞行研究
Free-flight investigation to determine the drag of flat - and vee - windshield canopies on a parabolic fuselage with and without transonic indentation between Mach numbers of 0.75 and 1.35