ThePelikan tail is an experimental tail design for fighter jets. It was originally conceived by Ralph Pelikan,[1] who was hired byMcDonnell Aircraft, later worked forMcDonnell Douglas after the merger of McDonnell with Douglas and, after another merger, retired fromBoeing. The concept was used in theNorthrop YF-23 fighter. However, it has been considered or included in design specifications in the McDonnell Douglas BAE Joint Strike fighter (JSF) design which was eliminated before prototype stage[2][3]
The Pelikan design differs from the typical layout offlight control surfaces andempennage (incorporatingailerons on the wing, ahorizontal stabilizer withelevators and avertical stabilizer with arudder), in that it uses only two moveable surfaces in order to achieve control ofpitch, yaw and roll. When evaluated by Boeing engineers in October 1998 while designing what became theX-32, they found advantages of greater pitch control at high angles of attack and that two tail surfaces would have a lower radar signature than the four surfaces eventually adopted.[1][2] However, they also found that using two larger control surfaces instead of four might actually make the aircraft heavier. The bigger hydraulic pumps and cylinders needed to operate the larger surfaces would add 800 to 900 pounds (360 to 410 kg) of weight to the design.[1] This and other factors made them use a four-surface tail instead.[1]
Virginia Tech students built a model aircraft with a Pelikan tail and got positive results for its viability using awind tunnel.[4] The analysis by the students found several advantagessuch as a lower vertical surface area, which aids in stealth; less drag due to skin friction; and a lower weight due to the need for two as opposed to the usual four hydraulic actuators.[failed verification][5]
