It is shown that when secondary effects are neglected, maximum available increase in lift due to power is equal to thrust being developed; if increase in lift due to power is expressed in coefficient form, very high values may be shown under conditions which are found to be wholly impracticable in flight.
Some fundamental considerations in regard to use of power in landing airplane
Nat Advisory Committee Aeronautics -- Tech Note
1939
7 pages
3 Supp sheets, Bibliography
Report
Englisch
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Engineering Index Backfile | 1931
|Engineering Index Backfile | 1931
|