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AMCOM/AFDD/TR-00-A-003 ARL-TR-2154 Wind Tunnel Evaluation of a Model Helicopter Main-Rotor Blade With Slotted (2001)  (Make Corrections)  
Joint Research Program Office Aeroflightdynamics Directorate U.S. Army...



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Abstract: this report is for accurate reporting and does not constitute an official endorsement, either expressed or implied, of such products or manufacturers by the National Aeronautics and Space Administration or the U.S. Army. Summary Data for rotors using unconventional airfoils are of interest to permit an evaluation of this technology's capability to meet the U.S. Army's need for increased helicopter mission effectiveness and improved safety and survivability. Thus, an experimental investigation... (Update)

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BibTeX entry:   (Update)

@misc{ program-amcomafddtr,
  author = "Joint Research Program",
  title = "AMCOM/AFDD/TR-00-A-003 ARL-TR-2154 Wind Tunnel Evaluation of a Model Helicopter
    Main-Rotor Blade With Slotted",
  url = "citeseer.ist.psu.edu/612576.html" }
Citations (may not include all citations):
6   Wind-Tunnel Evaluation of an Advanced Main-Rotor Blade Desig.. (context) - William, Jr et al. - 1987
6   Aerodynamic Characteristics of Two Rotorcraft Airfoils Desig.. (context) - Kevin - 1990
5   Aeroelastic Model Helicopter Rotor Testing in the Langley TD.. (context) - Wayne, Yeager et al. - 1985
3   SAWE Paper No (context) - Charles, in et al. - 1998
3   Performance and Vibratory Loads Data From a WindTunnel Test .. - William, Jr et al. - 1997
3   Important Scaling Parameters for Testing Model-Scale Helicop.. (context) - Jeffrey, Yeager et al. - 1998
2   Aerodynamic Characteristics of a Rotorcraft Airfoil Designed.. (context) - Kevin - 1991
2   Sharon: Investigation of a Slotted Rotorcraft Airfoil at Mac.. (context) - Kevin, Allison et al. - 1994

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