ICAS2016_0510: A CONCEPTUAL DESIGN PLATFORM FOR BLENDED-WING-BODY TRANSPORTS
A CFD Method of Reducing the Supersonic Drag Basing on the Area Rule Concept
Shock-Induced Separation Control by Using Nanosecond Pulsed SDBD Plasma Actuators (AIAA 2014-2368)
The Effect of PRF Fuel Octane Number on HCCI Operation
Experimental Study on HCCI Combustion of Dimethyl Ether(DME)/Methanol Dual Fuel
An Empirical Model of Nanosecond Pulsed SDBD Actuators for Separation Control
Novel scheme of OADM based on WDM demultiplexer, switch array, and OLM [3552-13]
Discussion of power management in an optical WDM network [3552-46]