Static Performance of Six Innovative Thrust Reverser Concepts for Subsonic Transport Applications: Summary of the NASA Langley Innovative Thrust Reverser Test Program (Google eBook)

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DIANE Publishing, 2000 - Aerodynamics - 366 pages
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Page 30 - Mercer, Charles E.; Berrier, Bobby L.; Capone, Francis J.; and Grayston, Alan M.: Data Reduction Formulas for the 16-Foot Transonic Tunnel-NASA Langley Research Center.
Page 1 - Results show that the innovative thrust reverser concepts achieved thrust reverser performance levels which, when taking into account the potential for system simplification and reduced weight, may make them competitive with, or potentially more cost effective than current state-of-the-art thrust reverser systems.
Page 30 - Test results have shown that several innovative thrust reverser concepts achieve thrust reverser effectiveness levels which, when considering the potential for system simplification and reduced weight, may make them competitive with the current state-of-art thrust reverser systems.
Page 30 - Poland, Dyckman T.: The Aerodynamics of Thrust Reversers for High Bypass Turbofans. AIAA 67-418, July 1967.

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