An aircraft propeller blade is constructed by forming two shells of composite material laminates and bonding the two shells to a metallic spar with foam filler pieces interposed between the shells at desired locations. The blade is then balanced radially and chordwise.
Method of making counterrotating aircraft propeller blades
20.11.1990
Sonstige
Keine Angabe
Englisch
Performance and Acoustic Prediction of Counterrotating Propeller Configurations
SAE Technical Papers | 1989
|The acoustic experimental investigation of counterrotating propeller configurations
Tema Archiv | 1987
|Application of momentum theory in counterrotating propeller design
IOS Press | 1971
|The Acoustic Experimental Investigation of Counterrotating Propeller Configurations
SAE Technical Papers | 1987
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