Wind Tunnel tests conducted on model with pod mounted turbojet engines operating for lift augmentation during landing and takeoff; measurement of longitudinal aerodynamic characteristics over angles of attack from -8 to 16° for momentum coefficients from 0 to 2.0 at several trailing edge flap deflections with half and full span flaps.
Aerodynamic characteristics, temperature, and noise measurements of large-scale external-flow jet-augmented-flap model with turbojet engines operating
NASA -- Tech Note
1961
46 pages
Report
English
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