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Flap (Aircraft) - Miller, Frederic P. (Hrsg.) / Vandome, Agnes F. (Hrsg.) / McBrewster, John (Hrsg.)
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Miller, Frederic P. (Hrsg.) / Vandome, Agnes F. (Hrsg.) / McBrewster, John (Hrsg.):
Flap (Aircraft) - pocketboek

2010, ISBN: 9786130674908

[ED: Taschenbuch / Paperback], [PU: Alphascript Publishing], Flaps are hinged surfaces on the trailing edge of the wings of a fixed-wing aircraft. As flaps are extended, the stalling speed of the aircraft is reduced, which means that the aircraft can fly safely at slower speeds (especially during take off and landing). Flaps are also used on the leading edge of the wings of some high-speed jet aircraft, where they may be called Krueger flaps. Extending flaps increases the camber of the wing airfoil, thus raising the maximum lift coefficient. This increase in maximum lift coefficient allows the aircraft to generate a given amount of lift with a slower speed. Therefore, extending the flaps will reduce the stalling speed of the aircraft. Extending flaps also increases drag. This can be beneficial in the approach and landing phase because it helps to slow the aircraft. Another useful side-effect of flap deployment is a decrease in aircraft pitch angle. This provides the pilot with a greater view over the nose of the aircraft and allows a better view of the runway during approach and landing. Some trailing edge flap systems increase the planform area of the wing in addition to changing the camber., DE, [SC: 0.00], Neuware, gewerbliches Angebot, 72, Selbstabholung und Barzahlung, PayPal, offene Rechnung, Banküberweisung, De internationale scheepvaart

Nieuw boek Booklooker.de
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Flap (Aircraft) - Miller, Frederic P. (Hrsg.) / Vandome, Agnes F. (Hrsg.) / McBrewster, John (Hrsg.)
uitverkocht boek
(*)
Miller, Frederic P. (Hrsg.) / Vandome, Agnes F. (Hrsg.) / McBrewster, John (Hrsg.):
Flap (Aircraft) - pocketboek

2010, ISBN: 9786130674908

[ED: Taschenbuch / Paperback], [PU: Alphascript Publishing], Flaps are hinged surfaces on the trailing edge of the wings of a fixed-wing aircraft. As flaps are extended, the stalling speed of the aircraft is reduced, which means that the aircraft can fly safely at slower speeds (especially during take off and landing). Flaps are also used on the leading edge of the wings of some high-speed jet aircraft, where they may be called Krueger flaps. Extending flaps increases the camber of the wing airfoil, thus raising the maximum lift coefficient. This increase in maximum lift coefficient allows the aircraft to generate a given amount of lift with a slower speed. Therefore, extending the flaps will reduce the stalling speed of the aircraft. Extending flaps also increases drag. This can be beneficial in the approach and landing phase because it helps to slow the aircraft. Another useful side-effect of flap deployment is a decrease in aircraft pitch angle. This provides the pilot with a greater view over the nose of the aircraft and allows a better view of the runway during approach and landing. Some trailing edge flap systems increase the planform area of the wing in addition to changing the camber., DE, [SC: 0.00], Neuware, gewerbliches Angebot, 72, Selbstabholung und Barzahlung, PayPal, offene Rechnung, Banküberweisung, Internationaler Versand

Nieuw boek Booklooker.de
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Verzendingskosten:Versandkostenfrei, Versand nach Deutschland (EUR 0.00)
Details...
(*) Uitverkocht betekent dat het boek is momenteel niet beschikbaar op elk van de bijbehorende platforms we zoeken.
Flap (Aircraft)
uitverkocht boek
(*)
Flap (Aircraft) - pocketboek

2010, ISBN: 9786130674908

[ED: Taschenbuch / Paperback], [PU: Alphascript Publishing], Flaps are hinged surfaces on the trailing edge of the wings of a fixed-wing aircraft. As flaps are extended, the stalling speed of the aircraft is reduced, which means that the aircraft can fly safely at slower speeds (especially during take off and landing). Flaps are also used on the leading edge of the wings of some high-speed jet aircraft, where they may be called Krueger flaps. Extending flaps increases the camber of the wing airfoil, thus raising the maximum lift coefficient. This increase in maximum lift coefficient allows the aircraft to generate a given amount of lift with a slower speed. Therefore, extending the flaps will reduce the stalling speed of the aircraft. Extending flaps also increases drag. This can be beneficial in the approach and landing phase because it helps to slow the aircraft. Another useful side-effect of flap deployment is a decrease in aircraft pitch angle. This provides the pilot with a greater view over the nose of the aircraft and allows a better view of the runway during approach and landing. Some trailing edge flap systems increase the planform area of the wing in addition to changing the camber., Neuware, gewerbliches Angebot

Nieuw boek Booklooker.de
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Flap (Aircraft) Wing, Fixed-wing aircraft, Stall (flight), Krueger flaps, Camber (aerodynamics), Lift coefficient, Drag (physics), Planform, True airspeed, Drag coefficient, Takeoff, Flight controls, Aileron - Miller, Frederic P. (Herausgeber); Vandome, Agnes F. (Herausgeber); McBrewster, John (Herausgeber)
uitverkocht boek
(*)
Miller, Frederic P. (Herausgeber); Vandome, Agnes F. (Herausgeber); McBrewster, John (Herausgeber):
Flap (Aircraft) Wing, Fixed-wing aircraft, Stall (flight), Krueger flaps, Camber (aerodynamics), Lift coefficient, Drag (physics), Planform, True airspeed, Drag coefficient, Takeoff, Flight controls, Aileron - nieuw boek

2010, ISBN: 6130674902

ID: A8294853

Kartoniert / Broschiert, mit Schutzumschlag neu, [PU:Alphascript Publishing]

Nieuw boek Achtung-Buecher.de
MARZIES.de Buch- und Medienhandel, 14621 Schönwalde-Glien
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Flap (Aircraft) Wing, Fixed-wing aircraft, Stall (flight), Krueger flaps, Camber (aerodynamics), Lift coefficient, Drag (physics), Planform, True airspeed, Drag coefficient, Takeoff, Flight controls, Aileron - Miller, Frederic P. (Herausgeber); Vandome, Agnes F. (Herausgeber); McBrewster, John (Herausgeber)
uitverkocht boek
(*)
Miller, Frederic P. (Herausgeber); Vandome, Agnes F. (Herausgeber); McBrewster, John (Herausgeber):
Flap (Aircraft) Wing, Fixed-wing aircraft, Stall (flight), Krueger flaps, Camber (aerodynamics), Lift coefficient, Drag (physics), Planform, True airspeed, Drag coefficient, Takeoff, Flight controls, Aileron - nieuw boek

2010, ISBN: 6130674902

ID: A8294853

Kartoniert / Broschiert, met couverture neu, [PU:Alphascript Publishing]

Nieuw boek Achtung-Buecher.de
MARZIES.de Buch- und Medienhandel, 14621 Schönwalde-Glien
Verzendingskosten:Geen versendingskosten in Duitsland. (EUR 0.00)
Details...
(*) Uitverkocht betekent dat het boek is momenteel niet beschikbaar op elk van de bijbehorende platforms we zoeken.

Bijzonderheden over het boek
Flap (Aircraft)

Flaps are hinged surfaces on the trailing edge of the wings of a fixed-wing aircraft. As flaps are extended, the stalling speed of the aircraft is reduced, which means that the aircraft can fly safely at slower speeds (especially during take off and landing). Flaps are also used on the leading edge of the wings of some high-speed jet aircraft, where they may be called Krueger flaps. Extending flaps increases the camber of the wing airfoil, thus raising the maximum lift coefficient. This increase in maximum lift coefficient allows the aircraft to generate a given amount of lift with a slower speed. Therefore, extending the flaps will reduce the stalling speed of the aircraft. Extending flaps also increases drag. This can be beneficial in the approach and landing phase because it helps to slow the aircraft. Another useful side-effect of flap deployment is a decrease in aircraft pitch angle. This provides the pilot with a greater view over the nose of the aircraft and allows a better view of the runway during approach and landing. Some trailing edge flap systems increase the planform area of the wing in addition to changing the camber.

Gedetalleerde informatie over het boek. - Flap (Aircraft)


EAN (ISBN-13): 9786130674908
ISBN (ISBN-10): 6130674902
Gebonden uitgave
pocket book
Verschijningsjaar: 2010
Uitgever: VDM Publishing House Ltd.

Boek bevindt zich in het datenbestand sinds 03.07.2007 19:29:16
Boek voor het laatst gevonden op 06.06.2018 10:29:35
ISBN/EAN: 9786130674908

ISBN - alternatieve schrijfwijzen:
613-0-67490-2, 978-613-0-67490-8


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