APA Citation

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

Chicago Style Citation

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

MLA Citation

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

Warning: These citations may not always be 100% accurate.