Numerical Assessment of Pneumatic Devices on the Wing/Fuselage Junction of a Tiltrotor

Author:

Simioni Nicola1,Ponza Rita1,Benini Ernesto2

Affiliation:

1. HIT09 S.r.l., 35131 Padova, Italy

2. Department of Industrial Engineering, University of Padova, 35131 Padova, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference27 articles.

1. ZalovcikJ. A.WetmoreJ. W.Von DoenhoffA. E. “Flight Investigation of Boundary Layer Control by Suction Slots on a NACA 35015 Airfoil at High Reynolds Numbers,” NACA, Rept. 4B29, Feb. 1944.

2. HeadM. R.JohnsonD.CoxonM. “Flight Experiments on Boundary Layer Control for Low Drag,” British Aeronautical Research Council, Rept. 3025, March 1955.

3. ClarkD. G. “Flight Development of a High Lift Research Aircraft Using Distributed Suction,” AGARD, Rept. 502, June 1965.

4. WagnerR. D.MaddalonD. V.FischerM. C. “Technology Developments for Laminar Boundary Layer Control on Subsonic Transport Aircraft,” AGARD P004-066, May 1984.

5. NASA and Boeing Commercial Airplane Group, “High Reynolds Number Hybrid Laminar Flow Control Flight Experiment, Suction System Design and Manufacture,” NASA CR-1999-209326, April 1999.

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