Horizontal Stabilizer Stability Thrust 
Pilot Institute
JUNE 4, 2025
A tailless aircraft is a fixed-wing airplane without a horizontal stabilizing surface. With this type of aircraft, the functions of longitudinal stability and control are incorporated into the main wing. A tailless airplane is one where everything needed to fly, like lift, control, and stability, is built into the main wing.
Vintage Aviation News
APRIL 11, 2025
They flew a total of 313 missions, collecting invaluable data on pitch stability, lift, drag, and buffeting in transonic and supersonic flight. Crossfield flew the Skyrocket 20 times, collecting critical data on longitudinal and lateral stability. After this conversion, it was launched from a Navy P2B (a modified B-29) at altitude.
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Vintage Aviation News
APRIL 18, 2025
The F-14s unique roll control setup, which relies on differential horizontal stabilizers and spoilers rather than traditional ailerons, provided effective control at various speeds but also introduced side forces that could contribute to spin entry.
Pilot Institute
JULY 11, 2025
When you reach around 36,000 feet (11,000 m) near the tropopause, the temperature stabilizes at around -56.5 °C. The tailplane (horizontal stabilizer) at high Mach can also develop shocks or experience disturbed airflow from the wings. on dry thrust alone. As you go higher, the air usually gets colder.
WayMan
MAY 25, 2025
The engine is what provides the thrust needed to move the aircraft forward. Propeller: Creating Thrust The propeller is an aerodynamic device that converts rotational motion into linear thrust. The angle and speed of the blades determine how much thrust is produced.
Aerotime
DECEMBER 27, 2024
The left winglet of one of the aircraft collided with the right horizontal stabilizer and elevator of the other. The aircraft sustained damage to the leading edge of the right-hand horizontal stabilizer and was subsequently repaired. The copilot selected the thrust reversers. degrees, the vertical load 2.47g.
Aerotime
MARCH 21, 2025
The pilot flyingpulled back the thrust levers, and as a result, over the following 5seconds, N1 decreased from 64% to approximately 43%, where it remained until touchdown. The engine thrust was steady at approximately 43%N1, the TSB report explained. The air speed began to decrease, the TSB report said.
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