Условие:
Two uniform equal stiff rods

and

are freely hinged at

and placed on a smooth horizontal table with

. A horizontal blow is delivered perpendicular to

at

. Find the ration of the resulting linear velocities of the centers of mass of

and of

, immediately after impact.
В русском условии
PNG в точке

не шарнир, а жесткое соединение. Хочу решить оригинальную задачу.
Согласно feynmanlectures.info/FLP_Original_Course_Notes/pages/ON2-043.html

,

и

взятые относительно центра масс в ускоряющейся системе.


Для стержня

:

, где

-- x-координата вектора силы, приложенной к точке

;

-- x-координата вектора силы с боку стержня

;

-- длина стержней,

;

-- масса любого стержня,

;

-- угловое ускорение по оси

, направленной перпендикулярно рисунку.
Ускорение точки

в системе центра масс

:


.
x-координата ускорения центра масс стержня

:

y-координата ускорения центра масс стержня

:

x-координата ускорения точки

в системе стола:

Для стержня

:


, где

-- x-координата силы , приложенной к стержню

с боку стержня

.
Получаем систему:

Отношение скоростей центров масс стержней:

Это правильный ответ?