Imaginactive's Paradoxal Aircraft Could Reach Supersonic Speeds

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Imaginactive's Paradoxal Aircraft Could Reach Supersonic Speeds

机译：Imaginactive的悖论飞机可以达到超音速

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Companies and organizations across the world continue to develop concepts that can one day transport passengers thousands of miles in just a few hours. But a company named Imaginactive could have the most impressive concept to date, named the Paradoxal.

机译：世界各地的公司和组织都在不断发展其概念，有一天可以在短短几个小时内将乘客运送数千英里。但是一家名为Imaginactive的公司可能拥有迄今为止最令人印象深刻的概念，即Paradoxal。

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《Unmanned systems》 |2017年第2期|44-44|共1页
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1. 2 supersonic aircraft programs reach testing milestones [J] . Litt Jonathan S., Conners Tim, Flamm Jeffrey D. Aerospace America . 2019,第11期

机译：2个超音速飞机计划达到测试里程碑
2. Low speed control of a second generation supersonic transport aircraft using integrated thrust vectoring [J] . A.J. Steer The Aeronautical Journal . 2000,第1035期

机译：使用集成推力矢量控制第二代超音速运输机的低速控制
3. The effect of supersonic aircraft speed on the penetration of sonic boom noise into the ocean [J] . victor W. Sparrow The Journal of the Acoustical Society of America . 1995,第1期

机译：超音速飞机的速度对音爆声噪声渗透到海洋中的影响
4. DRAG PREDICTION FOR SUPERSONIC CIVIL TRANSPORT AIRCRAFT AT LOW-SPEED, TRANSONIC AND SUPERSONIC CONDITIONS [C] . Gerald Carrier, Daniel Destarac CEAS Aerospace Aerodynamics Research Conference . 2002

机译：以低速，跨音速和超声波条件拖曳超音速民用运输机的预测
5. Sonic Boom Loudness Reduction through Localized Supersonic Aircraft Equivalent-Area Changes [D] . Abraham, Troy A. 2021

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6. Cooling Ability/Capacity and Exergy Penalty Analysis of Each Heat Sink of Modern Supersonic Aircraft [O] . Yu-Feng Mao, Yun-Ze Li, Ji-Xiang Wang, 2019

机译：现代超声波飞机每散热水槽的冷却能力/容量和漏斗罚款分析
7. Conceptual design of high speed supersonic aircraft: A brief review on SR-71 (Blackbird) aircraft [O] . Xue, Hui, Khawaja, Hassan Abbas, Moatamedi, Mojtaba 2014

机译：高速超音速飞机的概念设计：sR-71（黑鸟）飞机的简要回顾
8. Wind-tunnel Tests on an Aircraft Designed for Supersonic Speeds PART I High-speed Wind-tunnel Tests on 1/6.15-Scale Model Aircraft PART II No. 2 II1/2 -ft. Wind-tunnel Tests on a 1/4-Scale Model Wing [R] . S. P. HUTTON, M. Eng., A. D. Young 1950

机译：针对超音速设计的飞机的风洞测试第一部分1 / 6.15比例模型飞机的高速风洞试验第II部分第2号II1 / 2英尺。风洞测试1/4比例模型翼

Imaginactive's Paradoxal Aircraft Could Reach Supersonic Speeds

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