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What is solar system? Give some facts about solar system.
What is solar system? Give some facts about solar system.
planets

solar system

solar system defination

solar system facts

sun

Kisan Kumar Asked on 25th May 2020 in Astronomy.
- 1K views
- 1 answers
- 0 votes
Lift and Drag forces on aircraft
What are lift and drag forces in aircraft?
drag

drag force

lift

lift and drag

lift force

Worldtech Asked on 15th May 2020 in Aerospace.
- 1K views
- 1 answers
- 0 votes
treu-immo erfahrungen ist definitiv das Beste für erfahrene und neue Anfänger
Es gibt einige Arten von Bedingungen, mit denen ein Geschäftsmann im Geschäftsuniversum konfrontiert ist. Um die Probleme zu beseitigen, wenden …
Droekhat Asked on 27th April 2020 in None.
- 1K views
- 0 answers
- 0 votes
Sehr informative Details zu treu-immo.de
Jeder Unternehmer befasst sich mit vielen Herausforderungen innerhalb des Wettbewerbsuniversums, und zahlreiche Geschäftsleute verwenden verschiedene Ansätze, um die besonderen Probleme …
Droekhat Asked on 27th April 2020 in None.
- 1K views
- 0 answers
- 0 votes
Define absolute ceiling and service ceiling of an aircraft.
Define absolute ceiling and service ceiling of an aircraft.
Airplane design

flight mechanics

Kisan Kumar Asked on 31st December 2019 in Flight mechanics.
- 2K views
- 1 answers
- 0 votes
Consider an incompressible two-dimensional viscous flow over a curved surface. Let the pressure distribution on the surface be \(p(s)=2+sin\left ( \frac{\pi}{2}+s \right )\;N/m^2\),where \(s\) is the distance along the curved surface from the leading edge. Find the distance from where the flow separates.
Consider an incompressible two-dimensional viscous flow over a curved surface. Let the pressure distribution on the surface be \(p(s)=2+sin\left ( …
GATE

incompressible flow

Kisan Kumar Asked on 30th December 2019 in Aerodynamics.
- 1K views
- 1 answers
- 0 votes
Consider the superposition of a uniform flow 29 m/s, a source of strength 50m^2/s and a sink of strength –50m^2/s. The distance between the source and sink is 2m. Find the slenderness ratio of the Rankine oval, that is the ratio of the horizontal and vertical lengths for an oval shape.
Consider the superposition of a uniform flow 29 m/s, a source of strength 50 m^2/s and a sink of strength …
Aero Student Asked on 13th December 2019 in Aerodynamics.
- 1K views
- 1 answers
- 0 votes
Show the stagnation points
The lift coefficient on a spinning circular cylinder in a freestream with a velocity of 24 and at an altitude …
Aero Student Asked on 13th December 2019 in Aerodynamics.
- 1K views
- 0 answers
- 0 votes
What is the difference between an electronic violin and a traditional violin?
You still have to be able to master basic knowledge such as tuning, posture, grip and various disciplines that become …
dongtian Asked on 20th November 2019 in Others.
- 1K views
- 0 answers
- 0 votes
The measured lift slope for the NACA \(23012\) airfoil is \(0.1080\; degree^{−1}\), and \(α_{L}=0 = −1.3^{\circ}\). Consider a finite wing using this airfoil, with AR = \(8\) and taper ratio = \(0.8\). Assume that \(δ = τ\) . Calculate the lift and induced drag coefficients for this wing at a geometric angle of attack = \(7^{\circ}\).
The measured lift slope for the NACA \(23012\) airfoil is \(0.1080\; degree^{−1}\), and \(α_{L}=0 = −1.3^{\circ}\). Consider a finite wing …
airfoil

Airplane design

incompressible flow

Worldtech Asked on 12th November 2019 in Flight mechanics.
- 3K views
- 1 answers
- 0 votes

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