您的位置: 文献下载 » 科技会议 » 美国航空航天学会会议(AIAA) »

supportability considerations for advanced engine development

作者:科技文献资料网 时间:2018-10-16 10:17:03  浏览:8602   来源:科技文献资料网
下载地址: 点击此处下载
[唯一标识符]:CDSTIC.AIAA.1985-1205
[文献来源]:美国航空航天学会会议(AIAA)
[文献类型]:科技会议
[标题]:supportability considerations for advanced engine development
[作者]:files, j.s.
[出版单位]:美国航空航天局
[关键词]:Aircraft engines;Research &development;Aircraft maintenance;Tactical aircraft;Combat readiness;Maintainability;Design
[出版时间]:1985
[出版年份]:1985
[报告号]:AIAA85-1205
[馆藏索取号]:AIAA85-1205
[总页数]:6


下载地址: 点击此处下载
[文献类型]:科技报告
[标题]:A Collection of Papers in the Aerospace Sciences.
[作者]:nagaraja, k. s. petty, j. s.
[机构]:Air Force Aero Propulsion Lab.,Wright-Patterson AFB,OH.
[关键词]:aerodynamics,reports,propulsion systems,fluid dynamics,combustors,airframes,jet aircraft,aircraft engines,nozzles,ejectors,boundary layer flow,energy conservation,plasmas(physics),mathematical analysis,wind tunnels,aerospace science,papers,compilation reports,ntisdodxa
[出版年份]:1983
[报告号]:Rept no. AFAPL-TR-79-2126
[报告时间]:Jun 82,
[页码]:160p
[馆藏索取号]:AD-A122667
[总页数]:660


[文献类型]:科技报告
[标题]:Incidence Loss for Fan Turbine Rotor Blade in Two-Dimensional Cascade.
[作者]:kline, j. f. moffitt, t. p.
[机构]:National Aeronautics and Space Administration,Cleveland,OH. Lewis Research Center.
[关键词]:energy dissipation,fan blades,incidence,rotor aerodynamics,turbofan engines,two dimensional flow,aerodynamic characteristics,aspect ratio,cascade flow,flow visualization,kinetic energy,static pressure,velocity distribution,
[出版年份]:1983
[报告号]:NAS 1.60:2188, E-1587
[报告时间]:Jul 83,
[页码]:11p
[馆藏索取号]:N83-30431
[总页数]:12