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What is the role of horizontal stabilizer in an aircraft?
What is the role of horizontal stabilizer in an aircraft?
Aircraft performance

Airplane design

techAir Asked on 24th June 2020 in Flight mechanics.
- 2K views
- 1 answers
- 0 votes
What determines the length of a airport runway?
What determines the length of airport runway?
Aircraft performance

Airplane design

techAir Asked on 22nd June 2020 in Aeronautics.
- 1K views
- 1 answers
- 0 votes
What is the function of rudder in the aircraft?
What is the function of rudder in the aircraft?
Aircraft performance

Airplane design

Worldtech Asked on 22nd June 2020 in Aeronautics.
- 2K views
- 1 answers
- 0 votes
Poll Concorde airplane is
Concorde airplane is
Aircraft performance

Airplane design

Kumar59 Asked on 16th June 2020 in Aeronautics.
- 721 views
- 4 answers
- 0 votes
Poll The absolute ceiling of an aircraft is the altitude above which it
The absolute ceiling of an aircraft is the altitude above which it
Aircraft performance

flight mechanics

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Kisan Kumar Asked on 11th November 2019 in Flight mechanics.
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- 2 answers
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All the factors remaining constant, if the weight of an aircraft increases by $30 \%$ then the take off distance will increase by approximately.
All the factors remaining constant, if the weight of an aircraft increases by $30 \%$ then the take off distance …
Aircraft performance

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take-off distance

Kisan Kumar Asked on 10th November 2019 in Flight mechanics.
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- 1 answers
- 0 votes
Consider an NACA $2412$ airfoil with a $2\;m$ chord in an airstream with a velocity of $50\; m/s$ at standard sea level conditions. If the lift per unit span is $1353\; N$ , what is the angle of attack?
Consider an NACA $2412$ airfoil with a $2\;m$ chord in an airstream with a velocity of $50\; m/s$ at standard …
Aircraft performance

airfoil

Airplane design

incompressible flow

Worldtech Asked on 8th November 2019 in Aerodynamics.
- 2K views
- 1 answers
- 0 votes
Consider the data for the NACA $2412$ airfoil. Calculate the lift and moment about the quarter chord (per unit span) for this airfoil when the angle of attack is $4^{\circ}$ and the freestream is at standard sea level conditions with a velocity of $50 ft/s$ . The chord of the airfoil is $2 ft$ .
Consider the data for the NACA $2412$ airfoil. Calculate the lift and moment about the quarter chord (per unit span) …
Aircraft performance

airfoil

Airplane design

incompressible flow

Worldtech Asked on 8th November 2019 in Aerodynamics.
- 4K views
- 1 answers
- 0 votes
Poll Where is the zero pitching moment for an aircraft in trimmed condition?
An aircraft in trimmed condition has zero pitching moment at
Aircraft performance

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Kisan Kumar Asked on 30th September 2019 in Flight mechanics.
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- 1 answers
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What is the role of horizontal stabilizer in an aircraft?

What determines the length of a airport runway?

What is the function of rudder in the aircraft?

Poll Concorde airplane is

Poll The absolute ceiling of an aircraft is the altitude above which it

All the factors remaining constant, if the weight of an aircraft increases by 30 \%30 \% then the take off distance will increase by approximately.

Consider an NACA 24122412 airfoil with a 2\;m2\;m chord in an airstream with a velocity of 50\; m/s50\; m/s at standard sea level conditions. If the lift per unit span is 1353\; N1353\; N, what is the angle of attack?

Poll Where is the zero pitching moment for an aircraft in trimmed condition?

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All the factors remaining constant, if the weight of an aircraft increases by $30 \%$ then the take off distance will increase by approximately.

Consider an NACA $2412$ airfoil with a $2\;m$ chord in an airstream with a velocity of $50\; m/s$ at standard sea level conditions. If the lift per unit span is $1353\; N$ , what is the angle of attack?