Works matching DE "PIGGYBACK aircraft"

Results: 14

Effect of ply orientation on the in-plane vibration of single-layer composite plates.

Published in:: Noise & Vibration Worldwide, 2009, v. 40, n. 7, p. 43
Publication type:: Article

Aggregated Preference Value Analysis of Small Satellite Launch Opportunities.

Published in:

Transactions of the Japan Society of Aeronautical & Space Science, 2018, v. 61, n. 2, p. 69, doi. 10.2322/tjsass.61.69

By:

Mengying ZHANG;
Qin XU;
Qingbin ZHANG

Publication type:

Article

Multi-damage localization on large complex structures through an extended delay-and-sum based method.

Published in:

Structural Health Monitoring, 2016, v. 15, n. 1, p. 50, doi. 10.1177/1475921715623358

By:

Shan, Shengbo;
Qiu, Jinhao;
Zhang, Chao;
Ji, Hongli;
Cheng, Li

Publication type:

Article

Structural health monitoring–based methodologies for managing uncertainty in aircraft structural life assessment.

Published in:

Structural Health Monitoring, 2014, v. 13, n. 6, p. 621, doi. 10.1177/1475921714553733

By:

Bond, Ray;
Underwood, Sara;
Adams, Douglas E;
Cummins, Joshua J

Publication type:

Article

Part Qualification Methodology for Composite Aircraft Components Using Acoustic Emission Monitoring.

Published in:

Applied Sciences (2076-3417), 2018, v. 8, n. 9, p. 1490, doi. 10.3390/app8091490

By:

Esola, Shane;
Wisner, Brian J.;
Vanniamparambil, Prashanth Abraham;
Geriguis, John;
Kontsos, Antonios

Publication type:

Article

Probabilistic Design Methodology for Composite Aircraft Structure.

Published in:

Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2012, v. 44, n. 5, p. 683

By:

Chen Puhui;
Xiao Shanshan

Publication type:

Article

Non-Destructive Inspection of Impact Damage in Composite Aircraft Panels by Ultrasonic Guided Waves and Statistical Processing.

Published in:

Materials (1996-1944), 2017, v. 10, n. 6, p. 616, doi. 10.3390/ma10060616

By:

Capriotti, Margherita;
Kim, Hyungsuk E.;
Lanza di Scalea, Francesco;
Hyonny Kim

Publication type:

Article

System-on-Chip Integration of a New Electromechanical Impedance Calculation Method for Aircraft Structure Health Monitoring.

Published in:

Sensors (14248220), 2012, v. 12, n. 10, p. 13617, doi. 10.3390/s121013617

By:

Boukabache, Hamza;
Escriba, Christophe;
Zedek, Sabeha;
Medale, Daniel;
Rolet, Sebastien;
Yves Fourniols, Jean

Publication type:

Article

Experimental study of the effect of pre-bond contamination with de-icing fluid and ageing on the fracture toughness of composite bonded joints.

Published in:

Fatigue & Fracture of Engineering Materials & Structures, 2017, v. 40, n. 10, p. 1581, doi. 10.1111/ffe.12660

By:

Moutsompegka, E.;
Tserpes, K.I.;
Polydoropoulou, P.;
Tornow, C.;
Schlag, M.;
Brune, K.;
Mayer, B.;
Pantelakis, S.

Publication type:

Article

Foam.

Published in:: 2012
Publication type:: Product Review

TESTING | CHARACTERIZATION.

Published in:: Advanced Materials & Processes, 2018, v. 176, n. 1, p. 10
Publication type:: Article

Noise and vibration reduction technology in aircraft cabins.

Published in:

Advanced Composite Materials, 2004, v. 13, n. 1, p. 67, doi. 10.1163/1568551041408787

By:

Takahashi, Kosaku;
Monzen, Hirotaka;
Yamaoka, Toshihiro;
Kusumoto, Koji;
Bansaku, Kazuhiro;
Kimoto, Jyunichi;
Isoe, Akira;
Hirose, Yasuo;
Sanda, Tomio;
Matsuzaki, Yuji

Publication type:

Article

OPTIMIZATION OF COMPOSITE AIRCRAFT STRUCTURES IN CONSIDERATION OF POSTBUCKLING BEHAVIOR.

Published in:

International Journal of Structural Stability & Dynamics, 2010, v. 10, n. 4, p. 905, doi. 10.1142/S0219455410003804

By:

DAOUD, FERNASS;
CALOMFIRESCU, MIRCEA

Publication type:

Article

BUCKLING AND FAILURE OF COMPOSITE WEB.

Published in:

Aviation (1648-7788), 2003, v. 7, n. 1, p. 36

By:

Juračka, J.

Publication type:

Article