Distributed propulsion system

im getting thrust value 7-8N for rpm 1160 and 2500 both. how is that possible? can someone help me where nd what im doing wrong. the project is 2 propeller simulation on aircraft

Hi @anjalimistry3, thanks for posting! Please add a project link and a more detailed description as described here: Guide to Clear and Understandable Forum Posting

Cheers!
Igor