Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2019
ISBN 10: 6200287651 ISBN 13: 9786200287656
Librería: Books Puddle, New York, NY, Estados Unidos de America
EUR 85,20
Cantidad disponible: 4 disponibles
Añadir al carritoCondición: New.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2019
ISBN 10: 6200287651 ISBN 13: 9786200287656
Librería: preigu, Osnabrück, Alemania
EUR 47,85
Cantidad disponible: 5 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. Design and analysis of adaptive jet engine frame and thrust mounts | Jet engine frame and thrust mounts | S. Thangavel (u. a.) | Taschenbuch | 100 S. | Englisch | 2019 | LAP LAMBERT Academic Publishing | EAN 9786200287656 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing Sep 2019, 2019
ISBN 10: 6200287651 ISBN 13: 9786200287656
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
EUR 54,90
Cantidad disponible: 2 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -It is very essential to establish a multi jet engine test rig which can incorporate different types of jet engines in the same test rig. Such a test rig is called Universal Test Bed (UTB). The adaptive frame and thrust mounts are the important elements in the UTB. This project is carried out in Hindustan Aeronautics Ltd, Engine division. In this project an attempt has been made to design and analyze the adaptive frame and thrust mounts. This is done using geometric modeling and Finite Element Modeling. The above components are designed with the consideration of thrust force generated, weight of jet engine, self weight of test bed components and weight of air duct. The structural analysis is carried out to determine the stress level and deformation of the structure. 100 pp. Englisch.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2019
ISBN 10: 6200287651 ISBN 13: 9786200287656
Librería: Majestic Books, Hounslow, Reino Unido
EUR 86,28
Cantidad disponible: 4 disponibles
Añadir al carritoCondición: New. Print on Demand.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2019
ISBN 10: 6200287651 ISBN 13: 9786200287656
Librería: moluna, Greven, Alemania
EUR 45,45
Cantidad disponible: Más de 20 disponibles
Añadir al carritoCondición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Thangavel S.Mr.S.Thangavel working as Assistant Professor in the Department of Mechatronics Engineering, Kongu Engineering College, Erode. My current area of interest includes the design and fabrication sector in the automobile by in.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2019
ISBN 10: 6200287651 ISBN 13: 9786200287656
Librería: Biblios, Frankfurt am main, HESSE, Alemania
EUR 87,29
Cantidad disponible: 4 disponibles
Añadir al carritoCondición: New. PRINT ON DEMAND.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing Sep 2019, 2019
ISBN 10: 6200287651 ISBN 13: 9786200287656
Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemania
EUR 54,90
Cantidad disponible: 1 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -It is very essential to establish a multi jet engine test rig which can incorporate different types of jet engines in the same test rig. Such a test rig is called Universal Test Bed (UTB). The adaptive frame and thrust mounts are the important elements in the UTB. This project is carried out in Hindustan Aeronautics Ltd, Engine division. In this project an attempt has been made to design and analyze the adaptive frame and thrust mounts. This is done using geometric modeling and Finite Element Modeling. The above components are designed with the consideration of thrust force generated, weight of jet engine, self weight of test bed components and weight of air duct. The structural analysis is carried out to determine the stress level and deformation of the structure.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 100 pp. Englisch.
Idioma: Inglés
Publicado por LAP LAMBERT Academic Publishing, 2019
ISBN 10: 6200287651 ISBN 13: 9786200287656
Librería: AHA-BUCH GmbH, Einbeck, Alemania
EUR 55,56
Cantidad disponible: 1 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - It is very essential to establish a multi jet engine test rig which can incorporate different types of jet engines in the same test rig. Such a test rig is called Universal Test Bed (UTB). The adaptive frame and thrust mounts are the important elements in the UTB. This project is carried out in Hindustan Aeronautics Ltd, Engine division. In this project an attempt has been made to design and analyze the adaptive frame and thrust mounts. This is done using geometric modeling and Finite Element Modeling. The above components are designed with the consideration of thrust force generated, weight of jet engine, self weight of test bed components and weight of air duct. The structural analysis is carried out to determine the stress level and deformation of the structure.