Publikationsdatum:
2019-08-16
Beschreibung:
An investigation has been conducted in the Langley spin tunnel to determine the spin and recovery characteristics of a 1/20-scale model of the Northrop F-5E airplane. The investigation included erect and inverted spins, a range of center-of- gravity locations and moments of inertia, symmetric and asymmetric store loadings, and a determination of the parachute size required for emergency spin recovery. The effects of increased elevator trailing-edge-up deflections, of leading-edge and trailing-edge flap deflections, and of simulating the geometry of large external stores were also determined.
Schlagwort(e):
Aerodynamics
Materialart:
NASA-TM-SX-3556
,
L-11541
,
AF-AM-422
Format:
application/pdf
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