首页> 美国政府科技报告 >CAL/TRECOM SYMPOSIUM. PROCEEDINGS VOL. I. DYNAMIC LOAD PROBLEMS ASSOCIATED WITH HELICOPTERS AND V/STOL AIRCRAFT, JUNE 26-28, STATLER HILTON, BUFFALO, N. Y.
【24h】

CAL/TRECOM SYMPOSIUM. PROCEEDINGS VOL. I. DYNAMIC LOAD PROBLEMS ASSOCIATED WITH HELICOPTERS AND V/STOL AIRCRAFT, JUNE 26-28, STATLER HILTON, BUFFALO, N. Y.

机译:CaL / TRECOm sYmpOsIUm。诉讼VOL。 I.与直升机和V / sTOL飞机相关的动态负载问题,6月26日至28日,sTaTLER HILTON,BUFFaLO,N。Y.

获取原文

摘要

Contents: Dynamic loads in a rigid rotor from fullscale wind-tunnel tests,by J. F. Johnston, J. E. Rhodes,and R. H. Cotton;An aeroelastic study of helicopter rotor systems in high-speed flight,by E. R. Wood, K. D. Hilzinger,and A. C. Buffalano;In-flight measurement of steady and oscillatory rotor shaft loads,by R. Gabel;Full-scale flight test data relating to rotor unsteady aerodynamics,by Charles W. Ellis;Experimental and theoretical study of local induced velocities over a rotor disc,by S. Tararine;Rotor airloads,by R. Piziali, H. Daughaday,and F. DuWaldt;Comparison of flight measured helicopter rotor blade chordwise pressure distributions and two-dimensional airfoil characteristics,by James Scheiman and Henry Kelley; A discussion of rotor blade harmonic airloading,by R. H. Miller;An experimental investigation of the effect of a non-rigid wake on rotor blade airloads in transition flight,by Norman Ham.

著录项

相似文献

  • 外文文献
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号