高压捕获翼位置设计方法研究

李广利, 崔凯, 肖尧, 徐应洲 - 力学学报, 2016 - lxxb.cstam.org.cn
高压捕获翼构型是一种合理利用机体/上置翼(简称捕获翼) 间的耦合关系提高飞行器升力,
进而大幅提高升阻比的高速飞行器新概念构型. 基于其设计原理, 捕获翼的位置与机体压缩激波 …

The design method research for the position of high pressure capturing wing

L Guangli, C Kai, X Yao, X Yingzhou - 力学学报, 2016 - lxxb.cstam.org.cn
The high pressure capturing wing configuration is a novel conceptual form which improves
lift and lift-todrag ratios by the coupling relationship between the body and HCW. Based on …

hot-wire measurements of instability waves on a blunt cone at Mach-6

S Rufer, S Schneider - 35th AIAA Fluid Dynamics Conference and …, 2005 - arc.aiaa.org
Hot wire calibrations were completed in the supersonic jet facility at Purdue University. This
jet consists of a Mach-4 nozzle and allows for a continuous run time. The hot wires were …

Hot-wire measurements of instability waves on sharp and blunt cones at Mach 6

SJ Rufer - 2005 - search.proquest.com
Calibrated hot wires were used in the Mach-6 tunnel to obtain mass-flux profiles and to study
the amplitude and growth of instability waves on 7 half-angle sharp and blunt cones …

Hot-Wire Measurements of Instabilty Waves on Cones at Mach 6

S Rufer, S Schneider - 36th AIAA Fluid Dynamics Conference and …, 2006 - arc.aiaa.org
Hot wires were used in the Mach-6 tunnel to obtain mass flux profiles and to study the
amplitude and growth of instability waves on 7 half-angle sharp and blunt (0.020-inch …

[PDF][PDF] 平衡气体对乘波体气动力热特性影响

曾卫刚, 李维东, 王发民 - 空气动力学学报, 2012 - researchgate.net
针对乘波体在高空以高马赫数飞行时的特点, 给出了一种考虑高温平衡气体效应的乘波体设计
方法, 并通过数值模拟的方法研究了高空高马赫数飞行条件下高温平衡气体对乘波体气动特性的 …

Hypersonic laminar-turbulent transition experiment design: from wind tunnel model definition to MDOE approach

A Marino, R Fauci, R Donelli, A Schettino - 48th AIAA Aerospace …, 2010 - arc.aiaa.org
H= Enthalpy d= polynomial order K= Number of independent variables tα= Type I statistical
error tβ= Type II statistical error Re= Reynolds number Rext= Reynolds number calculated …

CFD Simulation of Power Law Bodies for Higher Mach Number Flows

VW Bhatkar, GV Shete… - … Journal of Vehicle …, 2024 - search.proquest.com
Hypersonic flight is of extreme interest today because of a new vehicle concept designed to
fly at very high Mach numbers. In hypersonic flows, strong shocks are generated with a …

[PDF][PDF] Slender Bodies at Hypersonic Speeds

PD Sonawane, N Mittal, GS Barpande… - IDST-MSAT2007 …, 2007 - researchgate.net
Hypersonic flight is of interest today because of new vehicle concepts designed to fly at a
very high Mach numbers. These concepts include trans-atmospheric vehicles, designed to …

[PDF][PDF] COLLEGE OF AERONAUTICS DEPARTMENT OF AEROSPACE SCIENCE

A Singh - 1996 - academia.edu
INTRODUCTION __________________________________… ver since the emergence of
human kind on planet Earth it has been striving for faster and faster means of transportation …