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In-cylinder Studies of Multiple Diesel Fuel Injection in a Single Cylinder Optical Engine
Chapter 23. Enhanced Communication to LEO Satellites
Development of an Integrated Propulsion and Pneumatic Power Supply System for Flapless UAVs
Integrated Design of a Model-Scale Gas Turbine Powered Flapless Demonstrator Aircraft: A Case Study
Designed Experiments for Nylon Band Characterization
In-cylinder studies of multiple diesel fuel injection in a single cylinder optical engine
A New Approach to Enhanced LEO Satellites Communication
Integrated Design of Fluidic Flight Controls for a Flapless Aircraft
Supersonic boundary-layer interactions with various micro-vortex generator geometries