Vintage Aviation News
APRIL 11, 2025
D-558-2 Skyrocket take off using JATO assist in 1949 NACA engineers improved the rockets performance by adding nozzle extensions to its combustion chambers, reducing exhaust interference with the rudders and increasing thrust at altitude. They also chilled the alcohol fuel and waxed the aircrafts fuselage to reduce drag for a record attempt.
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.
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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. Directional (yawing) stability from the vertical stabilizer. What Is a Tailless Aircraft? Lets find out.
Pilot Institute
JULY 11, 2025
The tailplane (horizontal stabilizer) at high Mach can also develop shocks or experience disturbed airflow from the wings. on dry thrust alone. As it accelerates, the Mach number increases further, which can make the shock and separation even worse, increasing the nose-down moment even more. It can supercruise above Mach 1.5
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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