Works matching IS 16487788 AND DT 2005 AND VI 9 AND IP 3
Results: 6
CRACK PROPAGATION IN RECTANGULAR THIN-WALLED PLATES WITH CONCENTRATORS SUBECTED TO CYCLING LOADING.
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- Aviation (1648-7788), 2005, v. 9, n. 3, p. 23, doi. 10.3846/16487788.2005.9635907
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- Article
INFLUENCE OF TRANSITION LOCATION ON AIRFOIL DRAG.
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- Aviation (1648-7788), 2005, v. 9, n. 3, p. 19, doi. 10.3846/16487788.2005.9635906
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- Article
APPLICATION OF GEOGRAPHICAL INFORMATION SYSTEMS IN MODELLING OF MILITARY OPERATIONS.
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- Aviation (1648-7788), 2005, v. 9, n. 3, p. 36, doi. 10.3846/16487788.2005.9635909
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- Article
GLOBAL ANALYSIS OF THE AIRCRAFT STRUCTURE AND ITS APPLICATION TO THE PRELIMINARY DESIGN STAGE.
- Published in:
- Aviation (1648-7788), 2005, v. 9, n. 3, p. 29, doi. 10.3846/16487788.2005.9635908
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- Article
NUMERICAL MODELING OF GAS TURBINE COOLED BLADES.
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- Aviation (1648-7788), 2005, v. 9, n. 3, p. 9, doi. 10.3846/16487788.2005.9635905
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- Article
MODEL OF ACOUSTIC EMISSION SIGNAL AT SELF-ACCELERATED CRACK DEVELOPMENT.
- Published in:
- Aviation (1648-7788), 2005, v. 9, n. 3, p. 3, doi. 10.3846/16487788.2005.9635904
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- Article