Srinivas, G., & Potti, S. R. (2014). Computational Analysis of Fighter Aircraft Wing under Mach Number 0.7 for Small Sweep Angles. Applied Mechanics and Materials, 592-594(Dynamics of Machines and Mechanisms, Industrial Research), 1020-1024. https://doi.org/10.4028/www.scientific.net/AMM.592-594.1020
Citácia podle Chicago (17th ed.)Srinivas, G., a Srinivasa Rao Potti. "Computational Analysis of Fighter Aircraft Wing Under Mach Number 0.7 for Small Sweep Angles." Applied Mechanics and Materials 592-594, no. Dynamics of Machines and Mechanisms, Industrial Research (2014): 1020-1024. https://doi.org/10.4028/www.scientific.net/AMM.592-594.1020.
Citácia podľa MLA (8th ed.)Srinivas, G., a Srinivasa Rao Potti. "Computational Analysis of Fighter Aircraft Wing Under Mach Number 0.7 for Small Sweep Angles." Applied Mechanics and Materials, vol. 592-594, no. Dynamics of Machines and Mechanisms, Industrial Research, 2014, pp. 1020-1024, https://doi.org/10.4028/www.scientific.net/AMM.592-594.1020.