Description: Report presenting an investigation made to improve compressor performance by bleedoff of detrimental boundary layer through a porous compressor casing. The results were compared to the performance characteristics of the original engine. Bleedoff was found to increase the efficiency of the compression process, but the overall performance of the turbojet suffered.
Date: December 11, 1953
Creator: Wlodarski, John
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department