16.100 Aerodynamics, Fall 2002 by Darmofal, David L.

Get full text

WGS.110 Sexual and Gender Identities, Fall 2010 by Surkan, K.J.

Get full text

SP.406 / WGS.406 Sexual and Gender Identities, Fall 2006 by Surkan, Kim

Get full text

Plastic Instability in Co-Cr-Ni-Mo alloy wires drawn with different drawing practices by GVK, Sai Srikanth, Tan, Ming Jen, Liu, Zhenyun

“…Plastic instability of Co-35Ni-20Cr-10Mo alloy was studied by inflicting the material to the different drawing process, namely Full Die Drawing (FDD) and Half Die Drawing (HDD). …”
Get full text

Aerodynamic optimization and drag minimization for the ultra low cost UAV piquero aerodynamic by Liu, Hao

“…The third segment is a full simulation of the Piquero UAV to determine its lift and drag characteristics. …”
Get full text

Exploring the drivers of bunker fuel prices by Yi, Yang Bo.

“…But not many pay attention to the drivers of bunker fuel price. There is scope therefore for further improvements in risk management in bunker purchasing. …”
Get full text

15.904 Strategic Management II, Fall 2003 by Hax, Arnoldo C.

Get full text

15.060 Data, Models, and Decisions, Fall 2002 by Freund, Robert Michael, Wang, Yashan, Bertsimas, Dimitris

Get full text

Injection effects on settling velocity by Le, Duc Anh

“…Settling is a process by which particulates that experience forces fall to the bottom of a liquid and form sediment at the vessel base. …”
Get full text

Numerical study of trapped vortex combustors characteristics in small ramjets by Chen, Song

“…The results show that the optimal cavity size that traps a vortex inside can be determined by calculating the drag coefficient. Because the designed small combustor does not have bypass air directed into the cavity, injecting all the fuel directly in the optimal cavity always leads to an overly fuel-rich condition. …”
Get full text

Wind tunnel testing of a ducted-fan unmanned aerial vehicle by Shiah, Zi Yang.

“…The experiments were carried out in a closed-loop wind tunnel with the full-scale MAV at different configurations. Coefficients of lift, drag and pitching moment were first discussed in a simple configuration of varying pitch angle with different wing setups without the propeller motor. …”
Get full text

Investigation of the effects of distributed propulsion over a flying body by Lee, Ann

“…One of the focuses in the current age is to reduce fuel consumption. Distributed propulsion systems show great potential in improving efficiency and achieving the goal of reducing fuel consumption. …”
Get full text

Aerodynamics of a wing body with different Winglet Cant Angle. by Bakhai, Mit Piyush, Mat, Shabudin, Musa, Nur Amalina

“…Current aircraft was designed with winglet at the tip. Winglets reduce the drag and improve fuel efficiency and range. The winglets have been in use for nearly 90 years, but it have been remained fixed. …”
Get full text

Numerical analysis on the aerodynamic characteristics of SUV car model install with vortex generator by Muhammad Amirul Hakimin, Zainondin, Izuan Amin, Ishak, Mohd Fuad, Yasak, Arafat, Mohammad, Nor Atiqah, Zolpakar, Nurshafinaz, Mohd Maruai

“…It is feasible to improve fuel efficiency by lowering the drag force. The study focuses on the influence of a vortex generator (VG) on the aerodynamics of a sport utility vehicle (SUV) car. …”
Get full text

PandoraHearts : Caucus Race, by Shinobu Wakamiya, author 655895, Jun Mochizuki, illustrator 655896

“…There, children run to and fro, full of life. Two cats chase after them. The sight calls to mind a single thought: They seem to be racing each other. …”
Get full text

Validation of ground effect drone by Dela Cruz, Joseph Eliz Ferdinand

“…Aerodynamic data including measurements of lift, drag, thrust, and other parameters will be tested, as well as an analysis of the vehicle's stability and control characteristics in both freestream and ground effect conditions. …”
Get full text

Comparative statics with adjustment costs and the Le Chatelier principle by Dekel, E, Quah, JK-H, Sinander, L

“…We show that comparative-statics conclusions may be drawn under the usual ordinal complementarity assumptions on the objective function, assuming very little about costs: only a mild monotonicity condition is required. …”

Load tests and moments evaluation of aircraft pylon using refurbished test assembly by Subas Chandrabose Satheesh Kumar

“…In this dissertation, a non-jettisonable pylon of F- 16 Aircraft used for carrying an external fuel tank or store (600 gallons capacity), is studied. …”
Get full text

Why travel far to learn? A study of environmental behaviour change experience of residential outdoor environmental education participants by Syed-Abdullah, Sharifah Intan Sharina

A model of intonational phonology of Singapore Malay by Diyana Hamzah

“…Intonation in Singapore Malay involves phrase-final rises, and an utterance-final rise-fall at the end of declaratives. The location of the utterance-final rise is dependent on the number of syllables of the final word. …”
Get full text