NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design of low Reynolds number airfoils. IILow Reynolds number airfoils were designed for high lift-to-drag ratios. Design considerations of low Re-airfoils are discussed and design examples are presented. It is shown that the performance of advance low Reynolds airfoils critically depends on proper laminar separation and transition control for the minimum profile drag coefficient with minimum turbulator device drag. This transition control close to the laminar separation is possible by enforcing transition on the upper surface either directly by means of spanwise rows of three-dimensional roughness elements, bleed or suction holes, or indirectly by means of destabilizing the upper surface boundary layer by means of backward facing surface steps, two-dimensional or zig-zag tapes or weak boundary layer blowing. Pneumatic turbulators are found to be advantageous because they can be adjusted to different external flow conditions better than mechanical ones.
Document ID
19880061707
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pfenninger, W.
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Vemuru, C. S.
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Mangalam, S.
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Evangelista, R.
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 88-3764
Meeting Information
Meeting: AIAA, ASME, SIAM, and APS, National Fluid Dynamics Congress
Location: Cincinnati, OH
Country: United States
Start Date: July 25, 1988
End Date: July 28, 1988
Accession Number
88A48934
Funding Number(s)
CONTRACT_GRANT: NAS1-18235
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available