Accession Number:

ADA517168

Title:

Impact of Airfoils on Aerodynamic Optimization of Heavy Lift Rotorcraft

Descriptive Note:

Conference paper

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MOFFETT FIELD CA AMES RESEARCH CENTER

Report Date:

2006-01-01

Pagination or Media Count:

12.0

Abstract:

Rotor airfoils were developed for two large tiltrotor designs, the Large Civil Tilt Rotor LCTR and the Military Heavy Tilt Rotor MHTR. The LCTR was the most promising of several rotorcraft concepts produced by the NASA Heavy Lift Rotorcraft Systems Investigation. It was designed to carry 120 passengers for 1200 nm, with performance of 350 knots cruise at 30,000 ft altitude. A parallel design, the MHTR, had a notional mission of 40,000 lb payload, 500 nm range, and 300 knots cruise at 4000 ft, 95 F. Both aircraft were sized by the RC code developed by the U. S. Army Aeroflightdynamics Directorate AFDD. The rotors were then optimized using the CAMRAD II comprehensive analysis code. Rotor airfoils were designed for each aircraft, and their effects on performance analyzed by CAMRAD II. Airfoil design criteria are discussed for each rotor. Twist and taper optimization are presented in detail for each rotor, with discussions of performance improvements provided by the new airfoils, compared to current technology airfoils. Effects of stall delay and blade flexibility on performance are also included.

Subject Categories:

  • Aerodynamics
  • VSTOL
  • Civilian Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE