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)
Experimental Study on HCCI Combustion of Dimethyl Ether(DME)/Methanol Dual Fuel
An Empirical Model of Nanosecond Pulsed SDBD Actuators for Separation Control
The Effect of PRF Fuel Octane Number on HCCI Operation
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]