Temperature distribution in the boundary layer of an airplane wing with a line source of heat at the stagnation edge. Part 1. Symmetric wing in symmetric flow

Yih, Chia-shun, 1918-1997, authorCermak, J. E. (Jack E.), authorShen, Richard Tsu-hsun, authorCivil Engineering Department, Colorado Agricultural and Mechanical College, publisher2017-09-292017-09-291952-10https://hdl.handle.net/10217/184170CER53CSY5.October, 1952.Includes bibliographical references.reportsengCopyright and other restrictions may apply. User is responsible for compliance with all applicable laws. For information about copyright law, please see https://libguides.colostate.edu/copyright.Boundary layerAirplanes -- WingsFluid dynamicsTemperature distribution in the boundary layer of an airplane wing with a line source of heat at the stagnation edge. Part 1. Symmetric wing in symmetric flowSymmetric wing in symmetric flowText