2024年9月8日 · The Finnish Air Force F/A-18 Hornet performs a brutal vertical takeoff at AIRPOWER 2024 in Zeltweg, that will blow you away! The intense roar of the engines,...

The McDonnell Douglas F/A-18 Hornet is an all-weather supersonic, twin-engine, carrier -capable, multirole combat aircraft, designed as both a fighter and attack aircraft (hence the F/A designation).

United States of America Navy Boeing F/A-18F Super Hornet 168890 at the Farnborough Airshow 2014 (not part of the flight programme)...more.

The tail configuration you have mentioned is usually referred to as canted vertical tails, since the vertical stabilizers are canted away from being 90° straight up and down. As illustrated in the below photo of the F-18 Hornet, this design has become increasingly common on modern military aircraft. Canted vertical stabilizers on the F-18

2003年3月1日 · A time-accurate computational analysis of vertical tail buffeting of full F/A-18 aircraft is conducted at typical flight conditions to identify the buffet characteristics of fighter aircraft. The F/A-18 aircraft is pitched at wide range of high angles of attack at Mach number of 0.243 and Reynolds number of 11 millions.

2015年8月23日 · The rudders are deflected inwards during takeoff of the F/A-18E to help in raising the nose of the aircraft as it leaves the ship. As the vertical fins are canted outwards, deflecting both the rudders inwards generates a downforce, which, due to its location aft of the center of gravity, creates a pitch-up moment.

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Explore how the F-18 achieves vertical takeoffs through thrust-to-weight ratio and wing design. Learn more about aviation physics and aerodynamics! #F18 #F18Hornet #AviationPhysics

Spatial Characteristics of F/A-18 Vertical Tail Buffet Pressures Measured in Flight Buffeting is an aeroelastic phenomenon which plagues high performance aircraft, especially those with twin vertical tails, at high angles of attack. Previous wind-tunnel and flight tests were conducted to characterize the buffet loads on the vertical tails by ...

2016年1月27日 · In the second phase, discussed in this paper, a Fluid Structure Interaction (FSI) tool was developed to permit unsteady aero-elastic simulations. Particular attention is focused on the vertical tail since this component of the F/A-18 fighter is very sensitive to fatigue due to unsteady loads generated by buffeting phenomena.