Forward-Flight Analysis of Slatted Rotors Using Navier-Stokes Methods

A study was conducted to evaluate the aerodynamic effects of leading-edge slats on rotor blades under high-speed forward-flight conditions. A partial-span leading-edge slat is proposed for the inboard porting of the existing UH-60A rotor.

Bibliographische Detailangaben

Veröffentlicht in:	Journal of aircraft 1997-01, Vol.34 (1), p.80-86
Hauptverfasser:	Bangalore, A, Sankar, L. N
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Applied sciences Exact sciences and technology Ground, air and sea transportation, marine construction Helicopters Miscellaneous transportation
Online-Zugang:	Volltext
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