Exact equivalence in results of momentum and vortex theory is shown; erroneous results may be incurred if inconsistent set of assumptions is used to formulate vortex theory.
Note on mean value of induced velocity for helicopter rotor
NASA -- Tech Note
1960
26 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Evaluation of induced-velocity field of idealized helicopter rotor
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