Rocket Propulsion Questions and Answers – Thrust Chambers – Heat Transfer Analysis
This set of Rocket Propulsion Multiple Choice Questions & Answers (MCQs) focuses on “Thrust Chambers – Heat Transfer Analysis”. 1. If dT/dL denotes temperature gradient with respect to thickness L at the surface A, k denotes the thermal conductivity, then the heat transferred per unit area is given by __________ a) Q/A = -k dT/dL … Read more