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Synonyms were used for: Composite • aircraft • fuselage • transport
Search without synonyms: keywords:(Composite transport aircraft fuselage)

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Contribution to an improved crash design for a composite transport aircraft fuselage—development of a kinematics model and an experimental component test setup

Waimer, M. / Kohlgrüber, D. / Keck, R. et al. | Online Contents | 2013

Keywords: Aircraft crashworthiness , Composite transport aircraft fuselage

Lightweight and reliable metal–composite joints based on harmonization of strength properties of joined parts

Chernov, Andrey / Fomin, Danil / Kondakov, Ivan et al. | SAGE Publications | 2018

Keywords: Composite structure , metal composite joint , aircraft structure , aircraft design , lattice composite structure , lattice composite fuselage

The crashworthiness prediction of 2D triaxially braided composite fuselage frame under transverse impact load

Ren, Yiru / Gao, Binhua / Liu, Xiaochuan et al. | Taylor & Francis Verlag | 2020

Keywords: aircraft , fuselage frame , braided composite

Dynamic testing and modelling of composite fuselage frames and fasteners for aircraft crash simulations

Heimbs, S. / Hoffmann, M. / Waimer, M. et al. | Tema Archive | 2013

Keywords: Verbundwerkstoff , Luftfahrzeug , Flugzeugrumpf

Aviation Safety: Status of FAA's Actions to Oversee the Safety of Composite Airplanes

NTIS | 2011

Keywords: Air Transportation , Transportation Safety , Aircraft , Composite Materials , Commercial aircraft , Composite materials , Fuselage

Contribution to an improved crash design for a composite transport aircraft fuselage—development of a kinematics model and an experimental component test setup

Waimer, M. / Kohlgrüber, D. / Keck, R. et al. | Springer Verlag | 2013

Keywords: Aircraft crashworthiness , Composite transport aircraft fuselage

Initial weight estimation of twin-fuselage configuration in aircraft conceptual design

Ma, Yiyuan / Yan, Jin / Elham, Ali | SAGE Publications | 2023

Keywords: aircraft conceptual design , Twin-fuselage configuration , composite materials

Initial Weight Estimation of Twin Fuselage Configuration in Aircraft Conceptual Design

Ma, Yiyuan / Yan, Jin / Elham, Ali | DataCite | 2021

Keywords: Twin fuselage configurati on, initial weight estimation, vortex lattice m ethod, composite materials, aircraft conceptual design

Einfluss elektromagnetisch absorbierender Folien auf Transferpfade in Luftfahrzeugen

Nunes, Rafael / Schüür, Jens | Tema Archive | 2014

Keywords: Luftfahrzeug , Flugzeugrumpf , Verbundwerkstoff

Crash concepts for CFRP transport aircraft – comparison of the traditional bend frame concept versus the developments in a tension absorbers concept

Waimer, M. / Feser, T. / Schatrow, P. et al. | Taylor & Francis Verlag | 2018

Keywords: Transport aircraft , composite material

Assessment of damage containment features of a full-scale PRSEUS fuselage panel

Bergan, Andrew / Bakuckas, John jun. / Awerbuch, Jonathan et al. | Tema Archive | 2014

Keywords: Flugzeugrumpf , Komposit , Luftfahrzeug , genadelter Verbundstoff

Development of a kinematics model for the assessment of global crash scenarios of a composite transport aircraft fuselage

Waimer, Matthias | Tema Archive | 2013

Keywords: Flugzeugrumpf , Kompositwerkstoff , Luftfahrzeug

Methodology for ecological and economical aircraft life cycle analysis

Große Böckmann, Markus / Schmitt, Robert | Tema Archive | 2012

Keywords: Luftfahrzeug , Flugzeugrumpf , Kompositwerkstoff , civil aircraft

CONSIDERATIONS IN SELECTION OF WING AND FUSELAGE SHEET MATERIALS FOR TRISONIC TRANSPORTS

Brown, W. F., Jr. / Espey, G. B. / Jones, M. H. et al. | NTRS | 1962

Keywords: FUSELAGE , TRANSPORT AIRCRAFT

A Short Brief on the Aircraft History and Anatomy

Ayar, Murat / Guleren, K. Melih | Springer Verlag | 2019

Keywords: Aircraft history , Timeline of aircraft , Fuselage , Transportation

Prüfmethode für Flugzeugrumpfschalen mit Kabellosen Sensoren für die Strukturüberwachung. Teilvorhaben. Verbundprojekt: Kabellose Sensoren für die Strukturüberwachung (CoolSensornet. Abschlussbericht. Prüfberichts-Nr.: C101/10.2. Auftrags-Nr.: 194129001. Berichtszeitraum: 01.02.2009 - 31.01.2012

Sachse, Mirko | Tema Archive | 2012

Keywords: Flugzeugrumpf , Verbundwerkstoff , Luftfahrzeug

Bulging Factor Solutions for Cracks in Longitudinal Lap Joints of Pressurized Aircraft Fuselages

A. Rahman / J. Bakuckas / C. Bigelow | NTIS | 2004

Keywords: Aircraft , Transport aircraft , Fuselage

Materials Examination of the Vertical Stabilizer from American Airlines Flight 587

M. R. Fox / C. R. Schultheisz / J. R. Reeder et al. | NTIS | 2005

Keywords: Transportation Safety , Aircraft , Composite Materials , Air Transportation , Commercial aircraft , Composite materials , Transportation

Modelling the impact behaviour of sandwich structures with folded composite cores

Kilchert, S. / Johnson, A.F. / Voggenreiter, H. | Tema Archive | 2014

Keywords: Komposit , Luftfahrzeug , Flugzeugrumpf

Initial Weight Estimation of Twin Fuselage Configuration in Aircraft Conceptual Design

Free access

Ma, Yiyuan / Yan, Jin / Elham, Ali | BASE | 2021

Keywords: Twin fuselage configurati on , composite materials , aircraft conceptual design