首页> 美国政府科技报告 >Tests of a 1/14-scale powered model of the XB-36 airplane in the Langley 19-foot pressure tunnel I : stalling characteristics and aileron effectiveness of several wing and flap arrangements

【24h】

Tests of a 1/14-scale powered model of the XB-36 airplane in the Langley 19-foot pressure tunnel I : stalling characteristics and aileron effectiveness of several wing and flap arrangements

机译：在Langley 19英尺压力隧道中测试XB-36飞机的1/14比例动力模型I：几个机翼和襟翼布置的失速特性和副翼效能

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
Sivells, James C;
展开▼
作者单位

展开▼
年度 1945
页码 1-21
总页数 21
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIRPLANES - CONSOLIDATED VULTEE B-36 (EXPERIMENTAL) WIND TUNNEL - TESTS (NACA -; STALLING CHARACTERISTICS - CONSOLIDATED VULTEE B-36; AILERONS - CONSOLIDATED VULTEE B-36; WING FLAPS, SLOTTED - PARTIAL-SPAN; WING FLAPS, FULL-SPAN; WING FLAPS, SPLIT - BALANCED; WINGS - CONSOLIDATED VULTEE B-36 WIND TUNNEL TESTS (NACA - PRESSURE-19'); WING SPOILERS;

机译：飞机 - 综合VULTEE B-36（实验）风洞 - 测试（NaCa - ;稳定特征 - 综合VULTEE B-36; aILERONs - 综合VULTEE B-36;翼形，开口 - 部分跨度;翼形，全跨度翼翼，分裂 - 平衡;翼 - 综合VULTEE B-36风洞试验（NaCa - pREssURE-19'）; WING spOILERs;
入库时间 2022-08-29 11:20:29

相似文献

外文文献

1. Wind tunnel tests for a flapping wing model with a changeable camber using macro-fiber composite actuators [J] . Kim DK, Han JH, Kwon KJ Smart Materials & Structures . 2009,第2期

机译：使用大型纤维复合执行器的可变外倾角襟翼机翼风洞测试
2. Wind Tunnel Testing Of Powered Lift, All-wing Stol Model [J] . S. W. Collins, B. W. Westra, J. C. Lin, Aeronautical journal . 2009,第1140期

机译：电动升降机全翼Stol模型的风洞测试
3. An Active Variable Camber Continuous Trailing Edge Flapped Wing Wind Tunnel Model for Aeroelastic 'In-Flight' Shape Optimization Tests [C] . Nathan Precup, Tyler Mundt, Marat Mor, . 2018

机译：主动可变弯度连续后缘拍打翼风洞模型用于气动弹性“飞行中”形状优化测试
4. Wind Tunnel Testing of Powered Lift, All-Wing STOL Model [O] . Jones Gregory S., Westra Bryan W., Zeune Cal H., 2008

机译：电动升降机全翼STOL模型的风洞测试
5. Tests of a 1/14-Scale Powered Model of the XB-36 Airplane in the Langley 19-Foot Pressure Tunnel. 1 - Stalling Characteristics and Aileron Effectiveness of Several Wing and Flap Arrangements [R] . Alexander, S. R., Sivelle, J. C. 1945

机译：1/14量表供电XB-36飞机的模型在兰利19足压隧道试验。 1 - 失速几个翼和襟翼安排的特点和副翼有效性

Tests of a 1/14-scale powered model of the XB-36 airplane in the Langley 19-foot pressure tunnel I : stalling characteristics and aileron effectiveness of several wing and flap arrangements

摘要

著录项

相似文献

相关主题

期刊订阅