首页> 美国政府科技报告 >Free-flight roll performance of a steady-flow jet-spoiler control on an 80 degree delta-wing missile between Mach numbers of 0.6 and 1.8

【24h】

Free-flight roll performance of a steady-flow jet-spoiler control on an 80 degree delta-wing missile between Mach numbers of 0.6 and 1.8

机译：在马赫数为0.6和1.8之间的80度三角翼导弹上的稳流喷射扰流控制的自由飞行滚转性能

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

No Abstract Available

著录项

作者
Schult, Eugene D;
展开▼
作者单位

展开▼
年度 1958
页码 1-39
总页数 39
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词

相似文献

外文文献
专利

1. A new high performance ionic liquid mixture electrolyte for large temperature range supercapacitor applications (-70 degrees C to 80 degrees C) operating at 3.5V cell voltage [J] . Newell Rodrigo, Faure-Vincent Jerome, Iliev Boyan, Electrochimica Acta . 2018,第期

机译：用于大型温度范围超级电容器的新型高性能离子液体混合物电解质（-70°C至80℃）以3.5V电池电压操作
2. Influence of the operational conditions on the performance of a chemisorption chiller driven by hot water between 65 degrees C and 80 degrees C [J] . de Oliveira Rogerio Gomes, Generoso Daniel Joao Applied Energy . 2016,第JANa15期

机译：运行条件对65°C至80°C热水驱动的化学吸附式制冷机性能的影响
3. A low-dimensional approach to closed-loop control of a Mach 0.6 jet Topics in Flow Control. Guest editors J.P. Bonnet and L. Cattafesta [J] . Low K.R., Berger Z.P., Kostka S., Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2013,第4期

机译：在流控制中以低维方法对0.6马赫喷射主题进行闭环控制的方法。客座编辑J.P. Bonnet和L.Cattafesta
4. A 0.6-V 1.8-#x03BC;W automatic gain control circuit for digital hearing aid [C] . Yu-Cheng Su, Shuenn-Yuh Lee, An-Po Lin IEEE Asia Pacific Conference on Circuits and Systems . 2008

机译：用于数字助听器的0.6V 1.8-μW自动增益控制电路
5. Introduction of control pins in the vicinity of missile fins for roll and yaw control. [D] . Pei, Jing. 2006

机译：在导弹鳍附近引入控制销，以进行侧倾和偏航控制。
6. Optimal Control Predicts Human Performance on Objects with Internal Degrees of Freedom [O] . Arne J. Nagengast, Daniel A. Braun, Daniel M. Wolpert 2009

机译：最佳控制可预测具有内部自由度的对象的人类性能
7. Aerodynamic interceptors efficiency for subsonic missiles roll attitude control [O] . Slobodan Mandić, Miloš Pavić, Bojan Pavković, 2017

机译：空气动力学拦截器对亚音导弹的效率滚动姿态控制

Free-flight roll performance of a steady-flow jet-spoiler control on an 80 degree delta-wing missile between Mach numbers of 0.6 and 1.8

摘要

著录项

相似文献

相关主题

期刊订阅