CFD Calculation of Helicopter Tail Rotor Airloads for Fatigue Strength Experiments-Reference-Cited by-同舟云学术

CFD Calculation of Helicopter Tail Rotor Airloads for Fatigue Strength Experiments

Published:2017-09 Issue:5 Volume:30 Page:04017032
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Janković D.¹,Maksimovic S.²,Kozic M.³,Stupar S.⁴,Maksimović K.⁵,Vasović I.⁶,Maksimovic M.⁷

Affiliation:

1. Research Assistant, VZ Moma Stanojlovic, Pukovnika Milenka Pavlovića 160, 11273 Belgrade, Serbia.

2. Professor, Military Technical Institute, Ratka Resanovica 1, Belgrade, Serbia.

3. Senior Research Associate, Military Technical Institute, Ratka Resanovica 1, Belgrade, Serbia.

4. Professor, Faculty of Mechanical Engineering, Kraljice Marije 16, Belgrade, Serbia.

5. Research Associate, City Administration of City of Belgrade, Secretariat for Utilities and Housing Services Water Management, Kraljice Marije 1, 11120 Belgrade, Serbia.

6. Research Associate, Institute Goša, Milana Rakica 35, Belgrade, Serbia; presently, Innovation Center Faculty of Mechanical Engineering, Univ. of Belgrade, Kraljice Marije 16, Belgrade, Serbia (corresponding author).

7. Research Associate, Belgrade Waterworks and Severage, Kneza Milosa 27, Belgrade, Serbia.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000734

Reference57 articles.

1. Advisory Group for Aerospace Research and Development Neuilly-Sur-Seine. (1973). “Specialist meeting on helicopter rotor loads prediction methods.” Agard Conf. Proc. No. 122 Milan Italy.

2. Anderson J. D. Jr. (1995). “Computational fluid dynamics.” The basics with applications McGraw-Hill New York.

3. An implicit upwind algorithm for computing turbulent flows on unstructured grids

4. Comparison of finite volume flux vector splittings for the Euler equations

5. ANSYS Release 15.0 [Computer software]. ANSYS Canonsburg PA.

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Efficient Computation Method for Total Fatigue Life of Aircraft Structural Components;Lecture Notes in Networks and Systems;2024

2. Strength Analysis of Helicopter Tail Rotor Blades Made from Composite Materials;Experimental Research and Numerical Simulation in Applied Sciences;2022-11-15

3. Computational Fluid Dynamics and Strength Analysis of Composite UAV Wing;Current Problems in Experimental and Computational Engineering;2021-11-19

4. Buckling and postbuckling behavior of shell type structures under thermo mechanical loads;Thermal Science;2021

5. Modeling of air and particles flow with revolving rotor hovering over the particles layer;Powder Technology;2020-10