Static stability and control characteristics are presented in form of 3-component force data obtained at from 5.8 to 10.1×106; data showing effects of thrust reversal on skin temperatures on fuselage and horizontal tail indicate that these effects were defined by ratio of reversed thrust to momentum of free stream.
Full-scale wind-tunnel investigation of effects of target-type thrust reverser on low-speed aerodynamic characteristics of single-engine jet airplane
NASA -- Tech Note
1959
42 pages
Report
Englisch
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Full-scale wind-tunnel tests of swept-wing airplane with cascade-type thrust reverser
Engineering Index Backfile | 1960
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