Present Status of Lateral-Control Devices for use with Split Flaps, Special Report (1933)
NASA Technical Reports Server (NTRS) · leaf 15
control at angles of attack above the stall is lost. Iho present plans are to continue flight tests to find the most forward spoiler location free from lag.. The next test will be made with the retractable-type spoilers near the trailing edge of the wing (fig. 8), whore they will give approximately… … Figure 8.- Eetractible spoilers.
NASA Technical Reports Server (NTRS)
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