Call Number (LC) Title Results
TL671.6 .F35 1969eb Fatigue design procedures : proceedings of the 4th symposium of the International Committee on Aeronautical Fatigue, held in Munich, 16-18 June 1965 / 1
TL671.6 .F39 1998 Application of the virtual crack closure technique to calculate stress intensity factors for through cracks with an oblique elliptical crack front / 1
TL671.6 .F68 1997 Practical stress analysis for design engineers : design and analysis of aerospace vehicle structures / 1
TL671.6 .G43 2008 Opportunities for systems engineering to contribute to durability and damage tolerance of hybrid structures for airframes / 1
TL671.6 .G65 2011eb Hybrid anisotropic materials for structural aviation parts
Hybrid anisotropic materials for structural aviation parts / 		3
TL671.6 .G67 Stress analysis for airplane draftsmen / 1
TL671.6 .G7 Flugzeugstatik / 1
TL671.6 .H565 2002 Introduction to structural dynamics and aeroelasticity / 1
TL671.6 .H565 2011eb Introduction to structural dynamics and aeroelasticity
Introduction to structural dynamics and aeroelasticity / 		4
TL671.6 .H57 1971 Aerostructures; selected papers of Nicholas J. Hoff / 1
TL671.6 .I23 2009 ICAF 2009 bridging the gap between theory and operational practice : proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, the Netherlands, 27-29 May 2009 / 1
TL671.6 .I23 2011 ICAF 2011 structural integrity influence of efficiency and green imperatives : proceedings of the 26th symposium of the International Committee on Aeronautical Fatigue, Montreal, Canada, 1-3 June 2011 / 1
TL671.6 .I23 2019eb ICAF 2019 -- Structural Integrity in the Age of Additive Manufacturing Proceedings of the 30th Symposium of the International Committee on Aeronautical Fatigue, June 2-7, 2019, Krakow, Poland / 1
TL671.6 .I5 1964 Acoustical fatigue in aerospace structures : proceedings of the Second International Conference. Dayton, Ohio, April 29-May 1, 1964 / 1
TL671.6 .I672 1993 Integrated airframe design technology Les technologies pour la conception integrée des cellules / 1
TL671.6 .K7 1995 Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods / 1
TL671.6 .K82 1956 Stresses in aircraft and shell structures. 1
TL671.6 .L597 1996 Structural loads analysis for commercial transport aircraft : theory and practice / 1
TL671.6 -- L597 1996eb Structural Loads Analysis : Theory and Practice for Commercial Aircraft. 1
TL671.6 .M36 Aircraft structures for engineering students / 1