Antony a Daniel (10 results)

Condition: New. In.

Condition: Very Good+.

Taschenbuch. Condition: Neu. Vibrational Analysis of Composite Vanes in Low Compressor Turbine | A. Daniel Antony | Taschenbuch | 72 S. | Englisch | 2020 | LAP LAMBERT Academic Publishing | EAN 9786202080361 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu.

Soft cover. Condition: Very Good. Moody, Burnett; V.K. Antony; et al (illustrator). Original colour illustrated wraps 22x28cm. Printed in Beirut by the Middle East Export Press. 32pp with b/w and colour photos and drawings. Very good. The cover story and much of the content presents a history of the American University of Beirut founded 100 years previously. Other content includes the poets and development of poetry at Ukaz (between Taif and Mecca); the work of oil dispatchers; Wadi Ram; and ancient Egyptian building. Photographers include Aramco's own Burnett Moody and V.K. Antony.

PAP. Condition: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.

PAP. Condition: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.

Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -In any gas turbine design cycle, blade design is a crucial element which needs maximum attention to meet the aerodynamic performance, structural safety margins, manufacturing feasibility, material availability etc. In present day gas turbine engines, most of the failures occur during engine development test and in-service, in rotor and stator blades due to fatigue and resonance failures. To address this issue, an extensive structural dynamic analysis is carried out to predict the natural frequencies and mode shapes using FE methods. Using the dynamics characteristics, the Campbell diagram is constructed to study the possibility of resonance at various operating speeds. In any rotating machinery, blade natural frequencies vary due to the centrifugal force and temperature over the speed range and it needs to be predicted accurately at design stages itself. At present, titanium alloy is used extensively for the blades which meet the structural requirements such as strength-weight ratio, manufacturing requirements and so on. In any aero gas turbine, weight reduction is of top priority with satisfactory structural reliability through extensive analysis and testing. 72 pp. Englisch.

Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Antony A. DanielMr. A. Daniel Antony - Assistant Professor. Specialization: Aircraft Stability Vibration, Aero-Elasticity.In any gas turbine design cycle, blade design is a crucial element which needs maximum attention to meet th.

Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -In any gas turbine design cycle, blade design is a crucial element which needs maximum attention to meet the aerodynamic performance, structural safety margins, manufacturing feasibility, material availability etc. In present day gas turbine engines, most of the failures occur during engine development test and in-service, in rotor and stator blades due to fatigue and resonance failures. To address this issue, an extensive structural dynamic analysis is carried out to predict the natural frequencies and mode shapes using FE methods. Using the dynamics characteristics, the Campbell diagram is constructed to study the possibility of resonance at various operating speeds. In any rotating machinery, blade natural frequencies vary due to the centrifugal force and temperature over the speed range and it needs to be predicted accurately at design stages itself. At present, titanium alloy is used extensively for the blades which meet the structural requirements such as strength-weight ratio, manufacturing requirements and so on. In any aero gas turbine, weight reduction is of top priority with satisfactory structural reliability through extensive analysis and testing.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 72 pp. Englisch.

Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - In any gas turbine design cycle, blade design is a crucial element which needs maximum attention to meet the aerodynamic performance, structural safety margins, manufacturing feasibility, material availability etc. In present day gas turbine engines, most of the failures occur during engine development test and in-service, in rotor and stator blades due to fatigue and resonance failures. To address this issue, an extensive structural dynamic analysis is carried out to predict the natural frequencies and mode shapes using FE methods. Using the dynamics characteristics, the Campbell diagram is constructed to study the possibility of resonance at various operating speeds. In any rotating machinery, blade natural frequencies vary due to the centrifugal force and temperature over the speed range and it needs to be predicted accurately at design stages itself. At present, titanium alloy is used extensively for the blades which meet the structural requirements such as strength-weight ratio, manufacturing requirements and so on. In any aero gas turbine, weight reduction is of top priority with satisfactory structural reliability through extensive analysis and testing.