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Kartei Details

Karten 59
Sprache English
Kategorie Technik
Stufe Universität
Erstellt / Aktualisiert 22.06.2016 / 22.06.2016
Lizenzierung Namensnennung - Nicht-kommerziell (CC BY-NC)    (Vorlesung Technikum)
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  1. When air passes through an oblique shock wave,

  1. Flow separation on an airfoil is caused by

  1. The critical Mach number for a wing increases when

  1. In straight and level flight, if the airspeed is doubled the induced drag

In general, when the wing trailing edge flaps are deflected

The airspeed for minimum power required

The static margin is defined as the distance between

In a coordinated turn with 60 bank, the stalling speed is approximately