论文信息 - Factors Shaping Conceptual Design of Rotary-Wing Aircraft - 字舞流文

Factors Shaping Conceptual Design of Rotary-Wing Aircraft

W. Z. Stepniewski

[1] L. G. Knapp. Multi Service Applications for Advancing Blade Concept Aircraft , 1980 .

[2] W. Z. Stepniewski,et al. Effect of at-the-source noise reduction on performance and weights of a tilt-rotor aircraft , 1975 .

[3] Dean E. Cooper. YUH‐60A Stability and Control , 1978 .

[4] F. H. Schmitz,et al. Full-Scale Measurements of Blade-Vortex Interaction Noise , 1982 .

[5] W Z Stepniewski. ENERGY ASPECTS OF HELICOPTERS IN COMPARISON WITH OTHER AIR AND GROUND VEHICLES , 1978 .

[6] W. Z. Stepniewski,et al. Possibilities and problems of achieving community noise acceptance of VTOL , 1973, The Aeronautical Journal (1968).