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

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.

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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
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Beschreibung
Zusammenfassung: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.
ISSN:0021-8669
1533-3868
DOI:10.2514/2.2138