Hyper-X flight engine ground testing for flight risk reduction
LD Huebner, KE Rock, EG Ruf, DW Witte… - Journal of Spacecraft …, 2001 - arc.aiaa.org
NASA'S Hyper-X program will advance technologies for vehicles utilizing hypersonic
airbreathing propulsion from the laboratory to the ight environment by obtaining data on a …
airbreathing propulsion from the laboratory to the ight environment by obtaining data on a …
Aerodynamic database development for the hyper-X airframe-integrated scramjet propulsion experiments
WC Engelund, SD Holland, CE Cockrell Jr… - Journal of Spacecraft …, 2001 - arc.aiaa.org
IN 1996 NASA initiated the Hyper-X Program, a jointly conducted effort by the NASA Langley
Research Center (LaRC) and the NASA Dryden Flight Research Center (DFRC), as part of …
Research Center (LaRC) and the NASA Dryden Flight Research Center (DFRC), as part of …
Hyper-X program status
C McClinton, V Rausch, J Sitz, P Reukauf - 39th Aerospace Sciences …, 2001 - arc.aiaa.org
This paper provides an overview of the objectives and status of the Hyper-X program, which
is tailored to move hypersonic, airbreathing vehicle technology from the laboratory …
is tailored to move hypersonic, airbreathing vehicle technology from the laboratory …
高超声速气动力数据天地相关性研究综述
陈坚强， 张益荣， 张毅锋， 陈亮中 - 空气动力学学报, 2014 - kqdlxxb.xml-journal.net
综述了国内外高超声速飞行器气动力数据天地换算技术方面的研究现状及趋势,
内容包括高超声速飞行器气动力地面试验研究进展, 气动力数值计算技术研究进展和试验数据 …
内容包括高超声速飞行器气动力地面试验研究进展, 气动力数值计算技术研究进展和试验数据 …
Aerodynamic study of the NASA's X-43A hypersonic aircraft
À Navó, JM Bergada - Applied Sciences, 2020 - mdpi.com
A 2D aerodynamic study of the NASA's X-43A hypersonic aircraft is developed using two
different approaches. The first one is analytical and based on the resolution of the oblique …
different approaches. The first one is analytical and based on the resolution of the oblique …
高超声速冲压发动机-飞行器计力体系讨论
白菡尘， 王泽江 - 推进技术, 2012 - jpt.tjjsjpt.com
从吸气式高超声速飞行器受力分析出发, 讨论如何统计飞行器受力的问题,
建议在研究中使用增量法. 这种方法将冲压发动机冷, 热工况产生的力(力矩) …
建议在研究中使用增量法. 这种方法将冲压发动机冷, 热工况产生的力(力矩) …
Optimization of hypersonic aircraft using genetic algorithms
V Ahuja, RJ Hartfield, A Shelton - Applied Mathematics and Computation, 2014 - Elsevier
A methodology has been developed to take advantage of hypersonic aircraft design
characteristics to allow design optimizations using computational fluid dynamics and genetic …
characteristics to allow design optimizations using computational fluid dynamics and genetic …
一体化高超声速飞行器气动-推进性能评估
贺元元， 倪鸿礼， 乐嘉陵 - 实验流体力学, 2007 - syltlx.com
吸气式高超声速飞行器的一个重要特点就是机体和推进系统的高度一体化设计.
在这类高超声速飞行器的发展中, 机体-推进系统内外流场相互干扰的评估以及飞行器气动 …
在这类高超声速飞行器的发展中, 机体-推进系统内外流场相互干扰的评估以及飞行器气动 …
Prediction of hyper-x stage separation aerodynamics using CFD
P Buning, TC Wong, A Dilley, J Pao - 18th Applied Aerodynamics …, 2000 - arc.aiaa.org
Abstract The NASA X-43" Hyper-X" hypersonic research vehicle will be boosted to a Mach 7
flight test condition mounted on the nose of an Orbital Sciences Pegasus launch vehicle …
flight test condition mounted on the nose of an Orbital Sciences Pegasus launch vehicle …
[PDF][PDF] 高超声速空间飞行器中若干非线性动力学问题进展
陈予恕， 钟顺， 郭虎伦 - 科学技术与工程, 2012 - stae.com.cn
摘# 要# 从国家对空间飞行器技术的需求出发, 综述空间飞行器中若干非线性动力学问题.
包括飞行器的连接结构, 液体燃料的晃动及其和整体结构的耦合, 以及气动弹性系统非线性等 …
包括飞行器的连接结构, 液体燃料的晃动及其和整体结构的耦合, 以及气动弹性系统非线性等 …