Главная страница

этапы отбора и ответы. Этапы отбора и ответы. REV2. Этапы отбора в Аэрофлот


Скачать 7.89 Mb.
НазваниеЭтапы отбора в Аэрофлот
Анкорэтапы отбора и ответы
Дата11.02.2020
Размер7.89 Mb.
Формат файлаdocx
Имя файлаЭтапы отбора и ответы. REV2.docx
ТипДокументы
#107966
страница9 из 57
1   ...   5   6   7   8   9   10   11   12   ...   57

Поляры верт. скоростей


At a given altitude, for any type of a/c excess power determines r/c. R/C changes with V. Graphs assist to determine max R/C and best A/C V.





If thrust available is constant with V (a jet engine). Maximum climb angle occurs at minimum drag.



For a jet or propeller, r/c max does not occur at minimum power required.

C max occurs at V where excess power is greatest.

The V for r/c max is found for any a/c by

  • Plotting both PR vs V and PA vs V

  • Finding the V where the distance between the PA and PR curves (excess) is the greatest



In general, PR decreases w/ altitude. And, PA drops faster than PR. R/C max decreases with altitude.





Ceiling is altitude where r/c has reached a limit.

1   ...   5   6   7   8   9   10   11   12   ...   57


написать администратору сайта