Zobrazeno 1 - 10
of 18
pro vyhledávání: '"I-Chung Chang"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2014 (2014)
The presented research validates the capability of a loosely coupled computational fluid dynamics (CFD) and comprehensive rotorcraft analysis (CRA) code to calculate the flowfield around a rotor and test stand mounted inside a wind tunnel. The CFD/CR
Externí odkaz:
https://doaj.org/article/024fde99d317428985718c9bee181dfc
Publikováno v:
The Journal of Physical Chemistry B. 110:3071-3077
A new type of surfactant with a hydrophile of dendritic polyethylenimine (C(12)(EI)(7)) was synthesized by a cationic polymerization of dodecylamine with aziridine and was used as a stabilizer to prepare Pt colloid, which is then used in situ to prep
Publikováno v:
International Journal of Aerospace Engineering, Vol 2014 (2014)
The presented research validates the capability of a loosely coupled computational fluid dynamics (CFD) and comprehensive rotorcraft analysis (CRA) code to calculate the flowfield around a rotor and test stand mounted inside a wind tunnel. The CFD/CR
Publikováno v:
Journal of Aircraft. 29:477-484
A numerical method is presented for calculating the unsteady transonic rotor flow with aeroelasticity effects. The blade structural dynamic equations based on beam theory were formulated by FEM and were solved in the time domain, instead of the frequ
Autor:
I-Chung Chang, R. Rajagopalan
Publikováno v:
21st AIAA Applied Aerodynamics Conference.
An axisymmetric, incompressible Navier-Stokes solver was developed to calculate the flow field of a ducted fan. The fan effect is modeled via the momentum source concept. The effects of the spinning fan blades were introduced into the flow field as t
Autor:
Anthony Cheng, Meng C. Li, P. T. Chu, C. K. Fang, Ho Ku Lan, H. C. Shiao, Grace H. Ho, I-Chung Chang, H. L. Yeh, C. Y. Huang, Chung-Jen Chen, K. Y. Shu, Y. C. Chu
Publikováno v:
SPIE Proceedings.
The lens heating (LH) induced focus drift of the ASML i-line Step & Scan was measured at five NA/Sigma settings: three ASML default and two TSMC production settings. The new LH scaling constants at three ASML settings, when multiplied by a dose-match
Publikováno v:
Aircraft Design and Operations Meeting.
This paper describes a new wing design code which is based on the Euler equations and a constrained numerical optimization technique. The geometry modification is based on a set of fundamental modes define on the unit interval. A design example invol
Publikováno v:
Journal of Physical Chemistry B; Feb2006, Vol. 110 Issue 7, p3071-3077, 7p
Autor:
I-Chung Chang, Chee Tung
Publikováno v:
25th AIAA Aerospace Sciences Meeting.
A new method is presented for calculating the quasi-steady transonic flow over a lifting or nonlifting rotor blade in both hover and forward flight by using Euler equations. The approach is to solve the Euler equations in a rotor-fixed frame of refer