AT first, I hate "
Mary Sue" style fanart or fanfiction heroines.
I respect the design of the C-37A "albatross" (albatrus) high-speed transport aircraft, but I had a doubt that the aircraft does not have a vertical tail and horizontal stabilizer.
Since large aircraft response to steering is slow, it will not be able to make these substitute thrust vector control or TVC nozzle as fighter.
In addition, transport aircraft lack of inherent stability of aircraft can lead to fatal consequences.
I upload her biography to my own webpage, a fictional leader of the aircraft designer, her name is "Ms. Blanche Fontaine" who is the female friend about Mr.George Sullivan.
Ms. Blanche Fontaine and her design group, they add the vertical tail, to add that the canard instead of the legacy normal horizontal tail to the fuselage due to the reason that the center of gravity is biased forward with respect to the wing in, she tome was to solve this problem.
Now "C-37B" Albatross (albatrus) complete.
Original design of the Boeing-McDonnell Defense Inc. [later designated variant type "A"]
A.D.2044 of the early summer, and beyond the Date of death age of George Sullivan, Ms. Blanche entering a prime of life of the 41-year-old, Boeing-McDonnell Defense, Inc. improvement of tactical high-speed transport aircraft C-37A Albatross (albatrus) of the problems has been developed is the other company from "the United Earth Expeditionary Force" (UEEF) was contracted.
Although the aircraft was originally large aircraft that has been developed by "the Army of the Southern Cross", their military request, by the collapse of the Southern Cross, the aircraft expedition fleet forces had been operating in the other planets had been operating in as it is requisitioned.
Airframe design which investigated the unreasonable high-speed performance in the (land based) Army native of "Anatole Eli Leonard" of interrupt, in order to reduce the air resistance to the extreme, a large aircraft that inherent stability is important, yet despite the investment objective of transport aircraft not even vertical tail rather than horizontal stabilizer, with unreasonable design that although there is no tail therefore dependent control of the horizontal stabilizer to thrust deflection (thrust vector control or TVC) nozzle, certainly high-speed performance is as a large aircraft was not protrude, steering stability is poor accident was a lot to handle spicy aircraft in.
The Army of the Southern Cross advanced in strict training spent also Saturday and Sunday, only had been visible from the outside as if they were operating seemingly normal, surviving veteran aviation soldiers of the old ASC is retired, the young do not know the Earth of UEEF When aviation is 2040's to take over the aircraft, serious death was frequently.
Fleet University and aviation technology headquarters, because of all of Boeing's offices in the earth within, by Invid occupation of 2033, from the fact that it is the company and the long-lost situation, Liège heavy industry and Blanche team design breaks the design of the aircraft We were ordered to the team.
Extraction of problems and solutions Blanche team. Have found the following problems, we went sequentially resolved
- The center of gravity is in the bias too forward with respect to the wing, the attachment of the horizontal stabilizer to the normal of the tail end is impossible.
- Initially of the design are allowed to substitute for the horizontal stabilizer in a two-dimensional thrust vectoring nozzle, this is a valid alternative method to small-sized aircraft such as fighter, the slow large aircraft of the reaction of the steering there is unreasonable, earlier I want the tail [canard].
- If the vertical tail of large aircraft also because replaced by small vertical small wings at both ends of the Wingtip device requires the area of the large vertical tail by the law of the square cube, it is impossible in some design. I want to add a bi-vertical tail to aft.
- Although of course the maximum speed of as Boeing-McDonnell Defence, Inc. self-propaganda high-speed transport aircraft is lowered due to an increase in air resistance, needed to transport aircraft is peaky, that is not a high-performance's or treat painful maneuvering performance, the range of movement of the inherent stability and the aerodynamic center of gravity of the aircraft It has to transport capacity, including.
Because there is no paper width, housed within the same paragraph the description of problems and solutions as a bullet, but was briefly summarized, this result will bear fruit in the image below.