MIT ChE Class 1966

MIT ChE Class 1966

MIT Chemical Engineering Class of 1966

The year 2016 makes the 50th anniversary of our class. From this inauspicious beginnings we rose as one group of individuals in our chosen profession in the mother country and our beloved USA. We became a part of a huge extended family, no matter the miles that separate us, yet find unity in a common experience and purpose.. Forever classmates...AMOR PATRIAE

Sunday, November 12, 2017






FLYING  AIRCRAFT CARRIER POWERED BY Turboelectric Distributed Propulsion Engine 

My conceptual design will be without the potruding nose but an upward deck where the planes can be launched in a 30 degree angle at the bow. The wings are fixed and a hybrid Blended Wing Body (BWB).
It will have two twin vertcal stabilizer situated halfway on the wings slanted outward from bow to aft, as the wings will be the whole length of the ship. All engines will be on the other side of the vertcal stabilizer allowing for a clean flight deck and safety for deck personnel.
Wing-mounted engines supply 80 per cent of the thrust required during take-off and 55 per cent at cruise. The tail-mounted all-electric (boundary-layer ingesting) BLI turbofan (pictured) accounts for the remaining thrust

Wing-mounted engines supply 80 per cent of the thrust required during take-off and 55 per cent at cruise. The tail-mounted all-electric (boundary-layer ingesting) BLI turbofan (pictured) accounts for the remaining thrust
In a conventional aircraft air clings to the body of the plane but with this new design air is transformed into power. To drive the fan (pictured), two smaller engines provide thrust

In a conventional aircraft air clings to the body of the plane but with this new design air is transformed into power. To drive the fan (pictured), two smaller engines provide thrust to develop unique vehicle concepts that will use different fuselage shapes; longer, skinnier and more blended wings. 



Placing the Engine The BWB program is examining a new method for engine installation that promises to increase safety and fuel efficiency. Three advanced “high-bypass ratio” engines will be buried in the trailing edge of the outer section of the BWB wing, allowing the center of the craft free for flight deck use. While conventional aircraft engines only take in “free-stream air,” both the air on and near the surface of the wing will flow through the BWB’s curved inlets and into its engines. Taking in the layer of air on the wing surface reduces drag. While this technology will require validation before becoming a reality, researchers are initiating tests to determine acceptable levels of turbulence in the engine inlet

Turboelectric Distributed Propulsion Engine Cycle Analysis for Hybrid-Wing-Body Aircraft




Keywords: soviet fold wing ocean landing floating flying aircraft carrier with landing pad illustration render by concept artist alface killah artstation.com portfolio image samples boac




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