AV
AV
AV
59
5.0 (1)
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) |
| Weblink |
https://card2brain.ch/box/pof1
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| Einbinden |
<iframe src="https://card2brain.ch/box/pof1/embed" width="780" height="150" scrolling="no" frameborder="0"></iframe>
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When air passes through an oblique shock wave,
Flow separation on an airfoil is caused by
The critical Mach number for a wing increases when
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
