Flight tests made over lift coefficient range up to about 12.5; characteristics of model without nose jet were satisfactory up to lift coefficient of about 4; of model with nose jet, they were satisfactory over test lift range, but control provided by conventional control surfaces was barely sufficient for maintaining flight at lift of 12.5.
Wind-tunnel investigation at low speeds of flight characteristics of sweptback-wing jet-transport airplane model equipped with external-flow jet-augmented slotted flap
NACA -- Tech Note
1958
32 pages
Article (Journal)
English
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