[1] 孙俊, 石岩峰, 凤蕴, 等. 20米地效翼船试验体系研究[J]. 船舶工程, 2008, 30(3):76-79. SUN J, SHI Y F, FENG Y, et al. Research of the test system of the 20 m wing-in-ground craft[J]. Ship Engineering, 2008, 30(3):76-79(in Chinese).
[2] BUTER E A. Wing-in-ground-effect vehicles[J]. Naval Engineers Journal, 1985(2):254-258.
[3] ROZHDESTVENSKY K V. Ekranoplan-Flying ships of the next century[C]//Second International Conference on Ekranoplans, 1995:47-70.
[4] KIRRILLOVIKH V N. Russian Ekranoplans[C]//Second International Conference on Ekranoplans, 1995:71-117.
[5] MALYSHEV M I. Experience of using Ekranoplans in Russia navy[C]//Second International Conference on Ekranoplans, 1995:233-244.
[6] 安东茂典. 米国DTNSRDCのPAR-WIG设计の基本思想[J]. 日本航空宇宙学会杂志, 1991, 39(448):14-22. ANTON S. The fundamental theory of the design of America PAR-WIG DTNSRDC[J]. Journal of the Aerospace Society of Japan, 1991, 39(448):14-22(in Japanese).
[7] 安东茂典, 加藤三千代. PAR-WIGの离水性能予测法[J]. 日本航空宇宙学会杂志, 1991, 39(455):38-46. ANTON S, KATO M. The prediction method of PAR-WIG on take-off performance[J]. Journal of the Aerospace Society of Japan, 1991, 39(455):38-46(in Japanese).
[8] 刘静. 地效飞机着水载荷数值分析[D]. 南京:南京理工大学, 2010. LIU J. The research on water load of wing-in-ground effect craft[D]. Nanjing:Nanjing University of Science and Technology, 2010(in Chinese).
[9] VON KARMAN T. The impact of seaplane float s during landing:NACA TN 321[R]. Washington, D.C.:National Advisory Committee for Aeronautics, 1929.
[10] WAGNER V H. Phenomena associated with impact s and sliding on liquid surfaces[J]. Z Angew Math Mech, 1932, 12(4):193-215.
[11] MONAGHAN R J, CREWE P R. Formulae for estimating the forces in seaplane-Water impacts without rotation or Chine immersion:NACA RN2804[R]. Washington, D.C.:National Advisory Committee for Aeronautics, 1949.
[12] MILLER R W. Theoretical analysis of hydrodynamic impact of a prismatic float having freedom in trim:NACA TN2698[R]. Washington, D.C.:National Advisory Committee for Aeronautics, 1952.
[13] SIM J L, SCHNITZER E. A theoretical investigation of the effect of partial wing lift on hydrodynamic landing characteristics of V-bottom seaplane in step impacts:NACA TN2815[R]. Washington, D.C.:National Advisory Committee for Aeronautics, 1952.
[14] WILLELM P. Theory of the landing impact of seaplanes:NACA TM624[R]. Washington, D.C.:National Advisory Committee for Aeronautics, 1931.
[15] STEINER M F. Analysis of planing data for use in predicting hydrodynamic impact loads:NACA TN1694[R]. Washington, D.C.:National Advisory Committee for Aeronautics, 1948.
[16] SCHNITZER E. Theory and procedure for determing loads and motions in Chine-Immersed hydrodynamic impacts of prismatic bodies:NACA TN2813[R]. Washington, D.C.:National Advisory Committee for Aeronautics, 1952.
[17] 褚林塘, 叶树林. 水上飞机文集[M]. 北京:航空工业出版社, 2011. CHU L T, YE S L. Collected works of seaplane[M]. Beijing:Aviation Industry Press, 2011(in Chinese). |