首页> 美国政府科技报告 >Summary of the lift, drag, and stability of 1/10-scale rocket-boosted models of the McDonnell XF3H-1 airplane for a Mach number range of 0.6 to 1.4 as affected by the operation of extensible rocket racks : TED No. NACA DE 351

【24h】

Summary of the lift, drag, and stability of 1/10-scale rocket-boosted models of the McDonnell XF3H-1 airplane for a Mach number range of 0.6 to 1.4 as affected by the operation of extensible rocket racks : TED No. NACA DE 351

机译：由于可扩展火箭架的操作影响，麦克唐纳XF3H-1飞机的1/10比例火箭增压型号的升力，阻力和稳定性概述，马赫数范围为0.6至1.4：TED No. NaCa DE 351

获取原文

页面导航

摘要
著录项
引文网络
相似文献
相关主题

摘要

No Abstract Available

著录项

作者
Crabill, Norman L; Mcfall, John C , Jr;
展开▼
作者单位

展开▼
年度 1954
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

1. Modeling of Lifted Turbulent Flame by the Flame Edge Theory and Its Implication in Liquid Rocket Combustion Instability [C] . J. Kim, S. Chung, J. Kim AIAA Aerospace Sciences Meeting and Exhibit . 2004

机译：火焰边缘理论模拟湍流升起火焰及其对液体火箭燃烧不稳定性的影响
2. The effects of extensible rocket racks on lift, drag, and stability of a 1/10-scale rocket-boosted model of the McDonnell XF3H-1 airplane for a Mach number range of 0.60 to 1.34 : TED No. NACA DE 31 [R] . Crabill, Norman L 1953

机译：可扩展火箭架对麦克唐纳XF3H-1飞机的1/10比例火箭增压模型的升力，阻力和稳定性的影响，马赫数范围为0.60至1.34：TED No. NaCa DE 31

Summary of the lift, drag, and stability of 1/10-scale rocket-boosted models of the McDonnell XF3H-1 airplane for a Mach number range of 0.6 to 1.4 as affected by the operation of extensible rocket racks : TED No. NACA DE 351

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅