9783330065529 - a Simple Way to Design & Construct an Airfoil by Mustak, Rubiat (6 results)
- Softcover
Seller: Revaluation Books, Exeter, United KingdomRevaluation Books
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Paperback. Condition: Brand New. 76 pages. 8.66x5.91x0.18 inches. In Stock.
- Softcover
Seller: preigu, Osnabrück, Germanypreigu
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£ 29.31
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Taschenbuch. Condition: Neu. A Simple Way to Design & Construct an Airfoil | Rubiat Mustak | Taschenbuch | 76 S. | Englisch | 2017 | LAP LAMBERT Academic Publishing | EAN 9783330065529 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu.
Language: English
Published by LAP LAMBERT Academic Publishing Mrz 2017, 2017
- Softcover
- Print on Demand
Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, GermanyBuchWeltWeit Ludwig Meier e.K.
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Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -When fluid flowing past an object tends to drag the object along in the direction of fluid flow. If an object is moving through a stationary fluid the drag tends to slow the object down. If the object is stationary in a flowing flui…d the drag tends to move the object in the direction of flow. While moving through air airplanes also subjected to several drags. In order to overcome these drags airplane wings cross section airfoils are designed very carefully. National Advisory Committee for Aeronautics or NACA developed and tested 'families' of airfoils. Some of the most successful of these were the NACA four-digit and five-digit series. The necessary coordinates for designing NACA airfoil profiles are available in online sources. But the present book describes the way of designing NACA four digit airfoils without taking any coordinates from available sources like google or any other search engines. Using C programming with the help of provided equations a generalized source code is designed. Which will provide coordinates for designing any NACA four digit airfoil profiles. 76 pp. Englisch.
- Softcover
- Print on Demand
Seller: moluna, Greven, Germanymoluna
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Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Mustak RubiatEngr. Rubiat Mustak completed his B.Sc in Mechanical Engineering from Khulna University of Engineering & Technology (KUET) in 2014. Currently he is contributing in the field of engineering…as well as research in the fiel.
Language: English
Published by LAP LAMBERT Academic Publishing Mär 2017, 2017
- Softcover
- Print on Demand
Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germanybuchversandmimpf2000
Contact seller5-star sellerCondition: New
£ 31.65
£ 51.35 shippingShips from Germany to U.S.A.Quantity: 1 available
Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -When fluid flowing past an object tends to drag the object along in the direction of fluid flow. If an object is moving through a stationary fluid the drag tends to slow the object down. If the object is stationary in a flowing fluid th…e drag tends to move the object in the direction of flow. While moving through air airplanes also subjected to several drags. In order to overcome these drags airplane wings cross section airfoils are designed very carefully. National Advisory Committee for Aeronautics or NACA developed and tested 'families' of airfoils. Some of the most successful of these were the NACA four-digit and five-digit series. The necessary coordinates for designing NACA airfoil profiles are available in online sources. But the present book describes the way of designing NACA four digit airfoils without taking any coordinates from available sources like google or any other search engines. Using C programming with the help of provided equations a generalized source code is designed. Which will provide coordinates for designing any NACA four digit airfoil profiles.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 76 pp. Englisch.
- Softcover
- Print on Demand
Seller: AHA-BUCH GmbH, Einbeck, GermanyAHA-BUCH GmbH
Contact seller5-star sellerCondition: New
£ 31.65
£ 51.92 shippingShips from Germany to U.S.A.Quantity: 1 available
Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - When fluid flowing past an object tends to drag the object along in the direction of fluid flow. If an object is moving through a stationary fluid the drag tends to slow the object down. If the object is stationary in a flowing fluid the… drag tends to move the object in the direction of flow. While moving through air airplanes also subjected to several drags. In order to overcome these drags airplane wings cross section airfoils are designed very carefully. National Advisory Committee for Aeronautics or NACA developed and tested 'families' of airfoils. Some of the most successful of these were the NACA four-digit and five-digit series. The necessary coordinates for designing NACA airfoil profiles are available in online sources. But the present book describes the way of designing NACA four digit airfoils without taking any coordinates from available sources like google or any other search engines. Using C programming with the help of provided equations a generalized source code is designed. Which will provide coordinates for designing any NACA four digit airfoil profiles.
