Preliminary performance data of several tail-pipe-cascade-type model thrust reversers
Description:
Report presenting the reverse-thrust performance of several tail-pipe-cascade-type model thrust reversers over a range of exhaust-nozzle pressure ratios from 1.2 to 2.4. Both symmetrical and asymmetrical cascade blade shapes were investigated. Results regarding the performance of tail-pipe-cascade-type model thrust reversers having symmetrically shaped cascade blades and the performance of tail-pipe-cascade-type model thrust reversers having asymmetrically shaped cascade blades are provided.
Date:
August 29, 1955
Creator:
Henzel, James G., Jr. & McArdle, Jack G.
Item Type:
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Partner:
UNT Libraries Government Documents Department