Theory is developed and numerical corrections are computed; at high speeds, corrections are same as those for wing; at low speeds, there is large upwash at rotor; numerical results for two wind-tunnel-wall configurations, one completely closed, and other closed on bottom only.
Jet-boundary corrections for lifting rotors centered in rectangular wind tunnels
NASA -- Tech Report
1960
91 pages
Report
Englisch
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Jet-boundary corrections for reflection-plane models in rectangular wind tunnels
Engineering Index Backfile | 1943
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