Have a personal or library account? Click to login
Validation of Numerical Models Used for Designing the Composite Blade for ILX-27 Rotorcraft Cover

Validation of Numerical Models Used for Designing the Composite Blade for ILX-27 Rotorcraft

Open Access
|Dec 2019

References

  1. [1] Szablewski K., Jancelewicz b., Łucjanek W., 1995, Introduction to rotorcraft design, Wydawnictwa Komunikacji i Łączności, Warszawa, (in Polish).
  2. [2] Kiraly R., Head R.E., 1983, Manufacturing Methods and Technology (MANTECH) Program: Manufacturing Techniques for Composite Main Rotor blade for the Advanced Attack Helicopter, united States Army Aviation Research and Development Command, St. Louis, MO.
  3. [3] Composite Materials Handbook – 17, ed., 2012, Composite Materials Handbook, Volume 3 – Polymer Matrix Composites – Materials usage, Design, and Analysis, Chapter 4, SAE International.
  4. [4] Feraboli P., 2009, Composite Materials Strength Determination Within the Current Certification Methodology for Aircraft Structures, Journal of Aircraft, Vol. 46, No. 4.10.2514/1.41286
  5. [5] Fawcett, A., Trostle, J., and Ward, S., 1977, 777 Empennage Certification Approach, 11th International Conference for Composite Materials, Melbourne, Australia.
  6. [6] Hodges D. H., 1990, Review of composite rotor blade modeling, AIAA Journal, 28 (3).10.2514/3.10430
  7. [7] bull J.W., Ed., 1996, Numerical Analysis and Modelling of Composite Materials, Springer Netherlands, Chapter 1: Analysis of composite rotor blades.10.1007/978-94-011-0603-0_1
  8. [8] Konik R, 2016, Numerical analysis of composite tail rotor blade, Transactions of the Institute of Aviation, No. 3(244), pp. 175-188, (in Polish).10.5604/05096669.1223407
  9. [9] Awrejcewicz j., Ed., 2011, Numerical Analysis – Theory and Application, InTech, Chapter 8: Numerical Validation Methods.10.5772/1829
  10. [10] Pyrzowski Ł., Sobczyk b., Witkowski W., Chróścielewski J, 2016, Three-point bending test of sandwich beams supporting the GFRP footbridge design process - validation, 3rd Polish Congress of Mechanics (PCM) / 21st International Conference on Computer Methods in Mechanics (CMM), Taylor & Francis Group.10.1201/b20057-104
  11. [11] Sears A. T., 1999, Experimental validation of finite element techniques for buckling and postbuckling of composite sandwich shells, MSc. Thesis, Montana State university, Bozeman.
  12. [12] ASTM International, 2016, Standard Test Method for Facing Properties of Sandwich Constructions by Long beam Flexure, ASTM D7249/D7249M − 16.
  13. [13] Kaddour A.S, Hinton M.J., 2012, Input data for for test cases used in benchmarking triaxial failure theories of composites, Journal of Composite Materials, No. 19-20/vol. 46; 2295-2312.10.1177/0021998312449886
  14. [14] Allen H.G., 1969, Analysis and Design of Structural Sandwich Panels, Pergamon Press, Oxford, UK.10.1016/B978-0-08-012870-2.50006-7
  15. [15] Zalewska M., 2017, Allowable values for the analysis of the spar of the main rotor blade for ILX rotorcraft: Roving AGY S2 Glass R-310 449, TEX 675, resin Araldite LY 1564/Aradur 2954, 4S/LK/2016 (in Polish), Institute of Aviation, Warsaw.
  16. [16] Karny M., 2016, Mechanical testing of tensile strength in 90° direction of the specimens made of glass roving in RTA conditions accoridng to ASTM D3039, 63/LK/2016, Institute of Aviation, Warsaw, (in Polish).
  17. [17] Zalewska M., 2016, Allowable values for the analysis of the casing of the main rotor blade for ILX rotorcraft for material MTM44-1/EHTA40(6k)-2x2T-284-40%, 5S/LK/2016, Institute of Aviation, Warsaw, (in Polish).
  18. [18] Evonik Industries, 2017, ROHACELL® WF Technical Information.
  19. [19] Quick Reference Guide: MSC Nastran, 2013.
Language: English
Page range: 23 - 31
Published on: Dec 26, 2019
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2019 Jakub Wilk, Radosław Guzikowski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.