Effects of Taper Ratio on the Longitudinal Characteristics at Mach Numbers From 0.6 to 1.4 of a Wing-Body-Tail Combination Having an Unswept Wing of Aspect Ratio 3 - Page 12 of 46 - UNT Digital Library
![An analysis of the effect that global taper ratio variations have upon compressively loaded asymmetric non-crimp fabric laminates incorporating realistically modelled transverse tapers - ScienceDirect An analysis of the effect that global taper ratio variations have upon compressively loaded asymmetric non-crimp fabric laminates incorporating realistically modelled transverse tapers - ScienceDirect](https://ars.els-cdn.com/content/image/1-s2.0-S1359836816301937-gr1.jpg)
An analysis of the effect that global taper ratio variations have upon compressively loaded asymmetric non-crimp fabric laminates incorporating realistically modelled transverse tapers - ScienceDirect
Effect of Taper Ratio on Lift, Drag, and Pitching-Moment Characteristics of Thin Wings of Aspect Ratio 3 With 53.1 Degrees Sweepback of Leading Edge at Subsonic and Supersonic Speeds - Page 17
26 Geometrical parameters of a wing [3] Taper ratio (λ), as a part of... | Download Scientific Diagram
![PDF] CFD Simulation of Different Taper Ratio Wings, Performing Trade-off Assessment and Development of A New Methodology to Plot Lift Distribution Curve and 3D Local Coefficient of Lift Distribution Graph | Semantic PDF] CFD Simulation of Different Taper Ratio Wings, Performing Trade-off Assessment and Development of A New Methodology to Plot Lift Distribution Curve and 3D Local Coefficient of Lift Distribution Graph | Semantic](https://d3i71xaburhd42.cloudfront.net/b70984efacbba75ab6d00734a283ca145b67240b/4-Figure5-1.png)