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Aerodynamic characteristics of a fighter model with a conventional delta wing and a cranked-tip delta wing at Mach numbers of 1.60 to 4.60

机译：具有传统三角翼和曲柄尖三角翼的战斗机模型的空气动力学特性，马赫数为1.60至4.60

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作者
Sorrells, R. B., III; Watson, C. B.;
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年度 1972
页码 1-142
总页数 142
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; AIRCRAFT MODELS; DELTA WINGS; EXTERNAL STORES; FIGHTER AIRCRAFT; MISSILES; TAIL ASSEMBLIES;

机译：空气动力学特征;飞机模型; DELTa WINGs;外部商店; FIGHTER aIRCRaFT;导弹; TaIL assEmBLIEs;

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专利

1. On the aerodynamic characteristics of thin slab delta wings at hypersonic speeds- part : effect of wing geometry [J] . R. Ramesh, B. Vasudevan, M.A. Ramaswamy The Aeronautical Journal . 2000,第1042期

机译：关于超音速薄板状三角翼的空气动力学特性-部分：机翼几何形状的影响
2. Optimization of Aerodynamic Parameters of Cropped Delta Wing with Fence at Sonic Mach Number [J] . M. P. Arun, M. Satheesh, J. Edwin Raja Dhas Journal of computational and theoretical nanoscience . 2019,第2期

机译：Sonic Mach数的围栏裁剪δ翼空气动力学参数的优化
3. STUDY OF MESH INDEPENDENCE ON THE COMPUTATIONAL MODEL OF THE ROLL-UP VORTEX PHENOMENON ON FIGHTER AND DELTA WING MODELS [J] . Setyawan Bekti Wibowo, Sutrisno, Tri Agung Rohmat Fluid mechanics research . 2019,第5期

机译：战斗机和三角翼模型卷起涡旋现象计算模型的网眼独立研究
4. Aerodynamic Analysis of a Generic Fighter with a Chine Fuselage/Delta Wing Configuration Using Delayed Detached- Eddy Simulation [C] . T. Jeans, U.S, D. McDaniel, AIAA Applied Aerodynamics Conference . 2008

机译：具有延迟机身涡流模拟的中机身/三角翼配置的通用战斗机空气动力学分析
5. A study of the nonlinear aerodynamic characteristics of a slender double-delta wing in roll. [D] . Pelletier, Alain. 1998

机译：横摇细长双三角翼的非线性空气动力特性研究。
6. Birds tails do act like delta wings but delta-wing theory does not always predict the forces they generate. [O] . Matthew R Evans 2003

机译：鸟的尾巴的确像三角翼但三角翼理论并不总是能预测它们产生的力。
7. Aerodynamic Analysis of a Generic Fighter with a Chine Fuselage/Delta Wing Configuration Using Delayed Detached-Eddy Simulation [O] . Jeans, Tiger L., McDaniel, David R., Cummings, Russell M., 2008

机译：具有延迟机身涡流模拟的中机身/三角翼配置的通用战斗机空气动力学分析
8. EFFECTS OF EXTERNAL STORES ON THE AERODYNAMIC CHARACTERISTICS OF A 60°DELTA-WING FIGHTER MODEL AT MACH 1.60 TO 2.87 [R] . M. Leroy Spearman, William J. Monta 1977

机译：外部存储对机床1.60至2.87的60°三翼机模型气动特性的影响

Aerodynamic characteristics of a fighter model with a conventional delta wing and a cranked-tip delta wing at Mach numbers of 1.60 to 4.60

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