APA (7th ed.) Citation

SHAMITHA, A., Crasta, A., Khan, S. A., & VASAVI, P. (2020). Computation of stability derivative for a wing for specific heat ratio= 1.66 for hypersonic flow. TJPRC Pvt. Ltd.

Chicago Style (17th ed.) Citation

SHAMITHA, A., Asha Crasta, Sher Afghan Khan, and P. VASAVI. Computation of Stability Derivative for a Wing for Specific Heat Ratio= 1.66 for Hypersonic Flow. TJPRC Pvt. Ltd, 2020.

MLA (9th ed.) Citation

SHAMITHA, A., et al. Computation of Stability Derivative for a Wing for Specific Heat Ratio= 1.66 for Hypersonic Flow. TJPRC Pvt. Ltd, 2020.