Search Results

Search Results

• Progressive failure analysis of helicopter rotor blade under aeroelastic loading

  Kamran Ahmad , Yasir Baig , Hammad Rahman , Hassan Junaid Hasham

  Abstract 1997 | PDF Downloads 1226 | DOI https://doi.org/10.3846/aviation.2020.12184

  Page 33-41
  

  2020-04-23

• Stress concentration factor of foamed materials used for cores of sandwich composites

  Daiva Zeleniakienė, Antanas Žiliukas

  Abstract 777 | PDF Downloads 632 | DOI https://doi.org/10.3846/16487788.2006.9635940

  Page 3-7
  

  2006-12-31

• Fuselage test of a small aircraft according to CS‐23 requirements

  Ivo Jebáček

  Abstract 767 | PDF Downloads 696 | DOI https://doi.org/10.3846/1648-7788.2009.13.26-33

  Page 26-33
  

  2009-03-31

• Research of the micromechanics of composite materials with polymer matrix failure under static loading using the acoustic emission method

  Aleksandrs Urbahs, Muharbijs Banovs, Kristine Carjova, Vladislav Turko, Jurijs Feshchuk

  Abstract 943 | PDF Downloads 648 | DOI https://doi.org/10.3846/16487788.2016.1264720

  Page 9-16
  

  2017-03-27

• Impact of variable geometry miniflaps on sailplane flight characteristics

  Peep Lauk, Karl-Erik Seegel, Toivo Tähemaa

  Abstract 1066 | PDF Downloads 1139 | DOI https://doi.org/10.3846/16487788.2017.1415228

  Page 119-125
  

  2017-12-21

• Crack propagation in rectangular thin‐walled plates with concentrators subected to cycling loading

  Henryk Kopecki, Jan Zacharzewski

  Abstract 696 | PDF Downloads 538 | DOI https://doi.org/10.3846/16487788.2005.9635907

  Page 23-28
  

  2005-09-30

• Fatigue indicators for metal structures: from aircraft to bridges

  Mykhailo Karuskevych , Tetiana Maslak , Oleg Karuskevych, Yurii Vlasenko

  Abstract 373 | PDF Downloads 180 | DOI https://doi.org/10.3846/aviation.2025.24532

  Page 174–182
  

  2025-09-29

• Mathematical models of the calculation of aircraft structural reliability

  Mykola Kulyk, Olexiy Kucher, Vladimir Miltsov

  Abstract 726 | PDF Downloads 572 | DOI https://doi.org/10.3846/16487788.2011.566315

  Page 11-20
  

  2011-04-14

• Interlaminar and intralaminar damage mechanisms of impact resistant aircraft materials under low‐energy impact

  Neringa Keršienė, Antanas Žiliukas

  Abstract 730 | PDF Downloads 676 | DOI https://doi.org/10.3846/16487788.2006.9635933

  Page 3-8
  

  2006-09-30

• Analysis of the results of acoustic emission diagnostics of a structure during helicopter fatigue tests

  Aleksandrs Urbahs, Kristine Carjova, Jurijs Fescuks

  Abstract 900 | PDF Downloads 734 | DOI https://doi.org/10.3846/16487788.2017.1335231

  Page 64-69
  

  2018-03-08

• Modal and random vibration analysis for structural design of aircraft external stores

  Linker Criollo , Carlos Mena-Arciniega , Juan Brazalez , Fabricio Medina , Marco Zurita

  Abstract 693 | PDF Downloads 400 | DOI https://doi.org/10.3846/aviation.2025.24456

  Page 137–149
  

  2025-09-12

• Mitigation of slivers using a new propellant grain design to improve propulsion systems

  Sarah Farrukh, M. Bilal Khan

  Abstract 838 | PDF Downloads 1107 | DOI https://doi.org/10.3846/16487788.2012.732320

  Page 76-83
  

  2012-10-02

• Reduction of the vibration in a helicopter blade using piezoelectric actuators

  Sergejs Gluhihs, Andrejs Kovalovs

  Abstract 716 | PDF Downloads 541 | DOI https://doi.org/10.3846/16487788.2006.9635927

  Page 3-6
  

  2006-06-30

• Efficiency of polymer materials in highly loaded systems in the aviation industry

  Anita Ptak, Tadeusz Leśniewski, Michał Purzycki, Krzysztof Płonka

  Abstract 689 | PDF Downloads 624 | DOI https://doi.org/10.3846/aviation.2023.20650

  Page 272–278
  

  2023-12-29

• Possibilities and methods of in-flight loading measurement

  Ivo Jebáček, Marek Horak

  Abstract 936 | PDF Downloads 953 | DOI https://doi.org/10.3846/16487788.2012.701860

  Page 47-50
  

  2012-06-29

• Investigation of dynamic stresses of tail beam of an MI‐8 helicopter

  Vitalijs Pavelko, Eric Ozolinsh, Ilmars Ozolinsh, Sergey Kuznetsov

  Abstract 708 | PDF Downloads 574 | DOI https://doi.org/10.3846/1648-7788.2008.12.118-123

  Page 118-123
  

  2008-12-31

• Identification and modelling process of defining temperature gradient in airport pavement

  Ervina Ahyudanari, Nasir Shafiq, Ibrahim Kamaruddin

  Abstract 860 | PDF Downloads 733 | DOI https://doi.org/10.3846/16487788.2014.926637

  Page 72-79
  

  2014-07-02

• Influence of miniflaps on sailplane flight characteristics

  Peep Lauk, Karl-Eerik Unt

  Abstract 830 | PDF Downloads 1111 | DOI https://doi.org/10.3846/16487788.2015.1104793

  Page 105-111
  

  2015-11-13

• Model of acoustic emission signal at the prevailing mechanism of composite material mechanical destruction

  Sergey Filonenko, Tatiana Nimchenko, Alexandr Kosmach

  Abstract 767 | PDF Downloads 472 | DOI https://doi.org/10.3846/aviation.2010.15

  Page 95-103
  

  2010-12-31

• Model of acoustic emission signal at self‐accelerated crack development

  Vitalii Babak, Sergay Filonenko, Viktor Kalita

  Abstract 790 | PDF Downloads 532 | DOI https://doi.org/10.3846/16487788.2005.9635904

  Page 3-8
  

  2005-09-30

• Modifications of a simple I-beam and its effects on the stress state

  Jakub Cejpek, Jaroslav Juračka

  Abstract 994 | PDF Downloads 696 | DOI https://doi.org/10.3846/16487788.2016.1227538

  Page 168-172
  

  2016-12-20

• Improved method for determining rheological parameters of composite materials during creep under torsional deformation

  Bidzina Abesadze , Saba Kopaliani

  Abstract 143 | PDF Downloads 80 | DOI https://doi.org/10.3846/aviation.2026.25922

  Page 24–32
  

  2026-02-23

• Raising gas-dynamic stability margin of axial and centrifugal compressor stages by means of vaned diffuser boundary layer control

  Ivan Lastivka

  Abstract 757 | PDF Downloads 656 | DOI https://doi.org/10.3846/16487788.2011.624262

  Page 76-81
  

  2011-10-04