X-35 LOW DRAG BODY
New! Bulk download of polars in Excel format: X-35%20LOW%20DRAG%20BODY.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
DB Name: X-35 LOW DRAG BODY
Family: Uncategorized
Max thickness: 20.6% at x = 58.01% chord
Max camber: 0.0% at x = 99.88% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
Notes:
Low drag axismmetric body presented in Parsons, Goodson, and Goldschmied, "Shaping of Axisysmmetric Bodies for Minimum Drag in Incompressible Flow", Journal of Hydronautics, Vol. 8 No. 3, July 1974.
https://arc.aiaa.org/doi/10.2514/3.48131