首页> 外文会议>AIAA/ASCE/AHS/ASC structures, structural dynamics and materials conference;AIAA SciTech forum >Full Scale Aircraft Drop Test Program for the F-35C Carrier Variant
【24h】

Full Scale Aircraft Drop Test Program for the F-35C Carrier Variant

机译:F-35C航母变型的全面飞机坠落测试程序

获取原文

摘要

The Lockheed Martin F-3S Lightning ( is a three variant family of single-seat, single-engine, all-weather, stealth multirole fighter aircraft currently in production for multiple US armed services and partner countries. The F-35C is the carrier variant design of the three variant family. Drop testing of a full scale structurally complete aircraft is required for verifying compliance with the US Navy structural integrity and flight certification requirements for the F-3SC carrier variant aircraft. The US Navy also requires a full scale drop test prior to clearing the aircraft to conduct high sink rate landings in flight test. The drop test program consisted of simulated shipboard landings for a variety of design touchdown conditions at specified aircraft attitudes, sink rates, and aircraft store configurations. The test objectives were to: (1) verify that structural integrity and functional design requirements for shipboard landing impacts have been met; and (2) collect loads and dynamics response data for correlation with analytical predictions. The F-35C drop test program successfully completed a total of 47 simulated shipboard landings without any structural failures and with good correlation between measured and predicted loads. The drop test results were used to clear the F-35C aircraft for shore-based carrier suitability flight testing and initial shipboard trials.
机译:洛克希德·马丁公司的F-3S Lightning(是三个型号的单座,单引擎,全天候,隐形多用途战斗机,目前正在为多个美国武装部队和合作伙伴国家生产。F-35C是航空母舰型号三个变体系列的设计,需要对全尺寸结构完整的飞机进行跌落测试,以验证是否符合美国海军对F-3SC航母变体飞机的结构完整性和飞行认证要求;美国海军也需要进行全尺寸跌落测试降落测试程序包括在指定的飞机姿态,下降率和飞机存放配置下,针对各种设计着陆条件的模拟舰载着陆,包括降落测试程序。 (1)验证是否满足船上着陆撞击的结构完整性和功能设计要求;以及(2)收集载荷和动力cs响应数据,用于与分析预测相关。 F-35C跌落测试程序成功完成了47个模拟舰载着陆,没有任何结构性故障,并且测得载荷与预测载荷之间具有良好的相关性。掉落测试结果用于清除F-35C飞机的岸基舰载机适合性飞行测试和初始舰载试验。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
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