3151.  Effects of collisional cooling on ion detection in a quadrupole ion trap mass spectrometer

Wu, H. F.; 吳慧芬; Brodbelt, J. S. ,  1992-05-01
[Graduate Institute & Department of Chemistry] Journal Article
International journal of mass spectrometry and ion processes 115, pp.67-81
establishes the ion trapping environment; the cooling time during which ions may collapse to the center of the trap; and the supplementary a.c. voltage used

3152.  Influences of plasma treatment and 6oCo γ - Ray radiation on the over-voltage positive temperature coefficient of high density polyethylene/carbon black nano composites

陳幹男 ,  2010-05-01
[Graduate Institute & Department of Chemical and Materials Engineering] Journal Article
Macromol. Symposia 286, pp.135-144
) and inorganic flame retardant (magnesium hydroxide, Mg(OH)2) was added. Influences of the CB content, plasma treatment time, plasma treatment power

3153.  Lossless data compression studies for the geostationary imaging Fourier transform spectrometer (GIFTS) with the bias-adjusted reordering preprocessing

Huang, Bormin; Wei, Shih-chieh; Huang, Allen H.-L.; Smuga-Otto, Maciek; Knuteson, Robert; Revercomb, Henry E.; Smith, William L. ,  2007-08
[Graduate Institute & Department of Information Management] Proceeding
Proceedings SPIE V. 6683
success of the GIFTS experiment where the data is to be disseminated to the user community in real-time and archived for scientific studies and climate

3154.  Dynamic fracture analysis of a finite crack subjected to an incident horizontally polarized shear wave

應宜雄; Ing, Yi-shyong; Ma, Chien-ching ,  1997-03-01
[Graduate Institute & Department of Aerospace Engineering] Journal Article
International journal of solids and structures 34(8), pp.895-910
meaning. The solutions are valid for an infinite length of time and have accounted for the contributions of an infinite number of diffracted waves

3155.  Numerical Analysis of heat transfer for Steady Three-Dimensional Compressible Flow in Long Microchannels

陳慶祥 ,  2005-06-01
[Graduate Institute & Department of Aerospace Engineering] Journal Article
Journal of Enhanced Heat Transfer 12(2), pp.171-188
. Experimentally, this was due to the difficulties in fabricating micro temperature sensors. Numerically, this was due to the long computational time

3156.  Flapping wings with PVDF sensors to modify the aerodynamic forces of a micro aerial vehicle

Yang, Lung-jieh; Hsu, Cheng-kuei; Ho, Jen-yang; Feng, Chao-kang ,  2007-04-09
[Graduate Institute & Department of Aerospace Engineering] Journal Article
Sensors and Actuators A: Physical 139(1-2), pp.95-103
with a range of 10–15 m. Finally, the MAV had a successful flight via wireless control with a range of 40 m and a total flight time of 10 s. 2007-04-09 en

3157.  A Reinterpretation of Empirical Mode Decomposition using Spectral Analysis Signal Reconstruction Method: Applications for Price Discovery of Futures and Spot Prices on WTI

張紘炬(Horng Jinh Chang); Pai, Ming-chu; Goo, Y. Jia; Hsu, Shih-chang ,  2011-03-01
[Department of Management Sciences] Journal Article
Advanced Institute of Convergence IT,vol.6, number 3,March 2011, P.132-145
as empirical objects, and applies [19] empirical mode decomposition (EMD). The EMD method decomposes the time sequence into several intrinsic mode functions

3158.  Development of a Non-contact Measurement System for In-situ Tool Profile Monitoring

Chao, C.L.; Cheng, T.A.; Lou, D.C.; Chao, C.W. ,  2006-11
[Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering] Journal Article
J. of C.C.I.T 35(1)
of time tool will experience attritious wear, micro-fracture and eventually worn out. Since the surface roughness and form accuracy are very much

3159.  Laser Propulsion System Performance Requirements for Single Stage to GEO Launch

Hong, Z. C.; Chern, C. Y.; Chern, J. S. ,  1995-01
[Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering] Journal Article
International Journal of Space Technology15(6), pp.395-401
system as a function of the flight time is solved. The initial mass of the launch vehicle is selected to be 10,000 kg. Its 10% is 1 ton and is the mass

3160.  Research on Fabricating CVD Diamond Microstructures Using RIE Process

Chou, Wen-chen; Chao, Choung-lii; Fan, Wei-haw; Ma, Kung-jeng ,  2009-02
[Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering] Journal Article, [Graduate Institute & Department of Computer Science and Information Engineering] Journal Article
Key Engineering Materials 407-408, pp.41-44
conditions, the irregular pillar-like microstructures started to emerge if the etching time was stretched longer. 2009-02 en Key Engineering Materials