9783330065529 - a simple way to design & construct an airfoil di mustak, rubiat (6 risultati)
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Da: Revaluation Books, Exeter, Regno UnitoRevaluation Books
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 74,48
EUR 11,68 spedizioneSpedito da Regno Unito a U.S.A.Quantità: 1 disponibili
Paperback. Condizione: Brand New. 76 pages. 8.66x5.91x0.18 inches. In Stock.
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Da: preigu, Osnabrück, Germaniapreigu
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 33,25
EUR 70,00 spedizioneSpedito da Germania a U.S.A.Quantità: 5 disponibili
Taschenbuch. Condizione: 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.
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Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, GermaniaBuchWeltWeit Ludwig Meier e.K.
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 35,90
EUR 23,00 spedizioneSpedito da Germania a U.S.A.Quantità: 2 disponibili
Taschenbuch. Condizione: 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 flu…id 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.
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Da: moluna, Greven, Germaniamoluna
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 31,27
EUR 48,99 spedizioneSpedito da Germania a U.S.A.Quantità: Più di 20 disponibili
Condizione: 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.
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Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germaniabuchversandmimpf2000
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 35,90
EUR 60,00 spedizioneSpedito da Germania a U.S.A.Quantità: 1 disponibili
Taschenbuch. Condizione: 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 t…he 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.
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Da: AHA-BUCH GmbH, Einbeck, GermaniaAHA-BUCH GmbH
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 35,90
EUR 60,66 spedizioneSpedito da Germania a U.S.A.Quantità: 1 disponibili
Taschenbuch. Condizione: 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 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.
