Thank you, ambivalent. It surely makes sense to look for smaller and cheaper aircraft carriers, but one has to take account of the arguments you mention.
I trained as an aircraft designer, not a naval architect. I am therefore aware of the advantage of having an aircraft launched with a vertical velocity component.
Now compare a monohull and a tricat with the same displacement. The tricat will have a greater length and a narrower main hull, a greater flight deck length and width.
The tricat needs more steel, has a greater wetted surface and a greater friction drag.
The tricat does not need internal bulges to protect the engines and magazines against torpedoes, as that is done by the side hulls.
Let's give both ships electric propulsion, GT or nuclear with GT get home power, and EM cats.
The monohull will have propellers close together, so their propulsive efficiency will be some 10 % lower then for a single screw vessel. I would imagine that the tricat with an propeller under each hull will pay a smaller penalty.
The tricat will have lower wave drag than the monohull, so at the speed for launching and recovering aircraft the power needed and thus the weight of the propulsion plant will be less.
The hangar forms the structure connecting the side hulls to the main hull and is as wide as the outside of the side hulls, with workshops on all sides and with elevators on every corner except the port aft corner.
The tricat will have a moderate ski jump with a pair of cats. Therefore aircraft are launched at about 80 % of the speed with which they need to leave a flat cat. This reduces the energy to be stored for a launch and the length of the cat by about a third.
The end of the landing strip is also a ski jump. so the pilot has, if he misses the arrester cables, more time to decide whether it is necessary to leave his office. The landing strip is also shorter.
So the tricat has a larger deck from which less space is occupied by launch and recovery areas.
It might well be that respotting of aircraft will occur less on the tricat than on the monohull.
The tricat has a larger structure weight but a lower propulsion plant weight, fuel weight,
I would imagine that the tricat configuration will be of no use to super carriers, but that a tricat carrier of halve the size and with halve the number of aircraft would be more effective than a monohull ( think CdG, QE2 ). It is something the Chinese might consider for carriers that start building after 2020.
I trained as an aircraft designer, not a naval architect. I am therefore aware of the advantage of having an aircraft launched with a vertical velocity component.
Now compare a monohull and a tricat with the same displacement. The tricat will have a greater length and a narrower main hull, a greater flight deck length and width.
The tricat needs more steel, has a greater wetted surface and a greater friction drag.
The tricat does not need internal bulges to protect the engines and magazines against torpedoes, as that is done by the side hulls.
Let's give both ships electric propulsion, GT or nuclear with GT get home power, and EM cats.
The monohull will have propellers close together, so their propulsive efficiency will be some 10 % lower then for a single screw vessel. I would imagine that the tricat with an propeller under each hull will pay a smaller penalty.
The tricat will have lower wave drag than the monohull, so at the speed for launching and recovering aircraft the power needed and thus the weight of the propulsion plant will be less.
The hangar forms the structure connecting the side hulls to the main hull and is as wide as the outside of the side hulls, with workshops on all sides and with elevators on every corner except the port aft corner.
The tricat will have a moderate ski jump with a pair of cats. Therefore aircraft are launched at about 80 % of the speed with which they need to leave a flat cat. This reduces the energy to be stored for a launch and the length of the cat by about a third.
The end of the landing strip is also a ski jump. so the pilot has, if he misses the arrester cables, more time to decide whether it is necessary to leave his office. The landing strip is also shorter.
So the tricat has a larger deck from which less space is occupied by launch and recovery areas.
It might well be that respotting of aircraft will occur less on the tricat than on the monohull.
The tricat has a larger structure weight but a lower propulsion plant weight, fuel weight,
I would imagine that the tricat configuration will be of no use to super carriers, but that a tricat carrier of halve the size and with halve the number of aircraft would be more effective than a monohull ( think CdG, QE2 ). It is something the Chinese might consider for carriers that start building after 2020.