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THEORETICAL PREDICTION OF THE FLOW IN THE WAKE OF A HELICOPTER ROTOR. ADDENDUM - EFFECTS DUE TO A FUSELAGE IN A CONSTANT, NONUNIFORM FLOW. 

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THEORETICAL PREDICTION OF THE FLOW IN THE WAKE OF A HELICOPTER ROTOR. ADDENDUM - EFFECTS DUE TO A FUSELAGE IN A CONSTANT, NONUNIFORM FLOW. 

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Attributes Comprehensive coverage

Label
PN
Publication Date
1966-01-01
Publisher
PN
Studio
PN
Lang
en-US

Product Identifiers

AID Algopix unique identifier
AID2AHQ56001
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