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DEVELOPMENT OF IN-FLIGHT MODULATING TYPE THRUST REVERSER FOR SINGLE ENGINE AIRCRAFT
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KEHRER, W., "DEVELOPMENT OF IN-FLIGHT MODULATING TYPE THRUST REVERSER FOR SINGLE ENGINE AIRCRAFT," SAE Technical Paper 600381, 1960, https://doi.org/10.4271/600381.Also In
References
- NASA Melo 4-26-59A “Flight Measurements of the Effect of a Controllable. Thrust Reverser on the Flight Characteristics of a Single-Engine Jet Airplane,” Anderson, Copper and Faye May 1959
- NASA TN D-72 “Full-Scale Wind Tunnel Investigation of the Effects of a Target-Type Thrust Reverser on the Low-Speed Aerodynamic Characteristics of a Single-Engine Jet Airplane,” Tolhurst, Kelly, and Greif Sept. 1959
- NACA TN 3665 “Performance and Operational Studies of a Full-Scale Jet Engine Thrust Reverser,” Kohl April 1956
- NACA TN 3975 “Investigation of a Full-Scale, Cascade-Type Thrust Reverser,” Kohl and Algrante April 1957
- NACA TN 3664 “Summary of Scale-Model Thrust Reverser Investigation,” Povolny, Steffen, and McArdle Feb. 1956
- NA-59-783 “Full-Scale Wind Tunnel Test of the F-100F Airplane with Thrust Reverser,” June 1959
- NASA TN D-311 “Full-Scale Wind Tunnel Tests of a Swept-Wing Airplane with a Cascade-Type Thrust Reverser,” Kelly, Greif, and Tolhurst April 1960
- NA-60-983 “F-100F Low Altitude Low Speed Control System - Final Flight Test Preport,” 8 August 1960