Principles of Flight (POF)
Principles of Flight FS 15 Klasse:AV14 Dozent:Manfrian Weiteres Lernmaterial unter: www.tinyurl.com/av14fs15
Principles of Flight FS 15 Klasse:AV14 Dozent:Manfrian Weiteres Lernmaterial unter: www.tinyurl.com/av14fs15
Set of flashcards Details
Flashcards | 126 |
---|---|
Students | 127 |
Language | English |
Category | Technology |
Level | University |
Created / Updated | 29.05.2015 / 14.04.2024 |
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In general adding a fuselage to a wing shifts the aerodynamic center ....
In general adding a fuselage to a wing shifts the aerodynamic center forward, .... the lift curve slope
In general adding a fuselage to a wing contributes a ... increment to the moment about the aerodynamic center.
the tail volume ratio is ...
the ratio between a volume wich defines the position and size of the tail and a volume which charaterizes the size of the wing.
the tail setting angle \(i_t\) must be ... to balance the airplane
if the center of gravity is at the neutral point ....
the airplane is statically neutral.
if the center of gravitiy is behind the neutral point
the airplane is statically unstable
if the center of gravitiy is infront of the neutral point
the airplane is statically stable
Define the elevator control effectivenes
It is the slope of the curve, Lift coefficient of the tail ploted versus the elevator downward deflection angle at a constant angle of attack.
it is always positive
what is the goal of elevator deflection
to maintain the airplane trimmed at different velocitys, and different angle of attacks.
By deflecting the elevator the moment coefficient curve gets shifted to the left or to the right.
Definition of Pressure
Pressure is the Force perpendicular to a surface per area
Pressure at sea level \(p_s =101325 N/m^2\)
Definition of density
Density is mass contained in a volume divided by that volume
Density at Sea level \(\rho_s=1.225 kg/m^3\)
0 Grad Celsius in Kelvin
273.15
speed is a ....
scalar
velocity is a .....
vector
A flow is incompressible if
\(V< ...m/s\)
100 m/s
What is an isentropic flow
An isentropic flow is adiabatic (no heat exchange) and reversible (no friction or other dissipative effects, production of entropy)
what is adiabatic
a prozess in which no heat is added or taken away
what is a reversible process
a process in which no entropy is produced (impossible)
A flow is incompressible if:
\(V< M....\)
Mach 0.3
In our course we asume that the flow through a sound wave is ....
if M=1.0 the flow is....
the flow is sonic
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