Based on experience from flight tests of swept aircraft, possible methods are discussed for determining, from wind tunnel test, maximum obtainable lift coefficient for landing; this is found difficult since dynamic effects in actual flight are not present in wind tunnel; based on available wind tunnel data approximate calculation of obtainable lift for landing is carried through for swept wing aircraft with various wing planforms; prevention of tip stall.
Maximum lift for landing of swept wing aeroplanes
Svenska Aeroplan Aktibolaget -- Tech Note
1953
14 pages
Report
Englisch
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Maximum lift for landing of swept wing aeroplanes
TIBKAT | 1953
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