Commuter aircraft aerodynamic characteristics through wind tunnel tests-Reference-Cited by-同舟云学术

Commuter aircraft aerodynamic characteristics through wind tunnel tests

Published:2016-07-04 Issue:4 Volume:88 Page:523-534
ISSN:0002-2667
Container-title:Aircraft Engineering and Aerospace Technology
language:en
Short-container-title:Aircraft Eng & Aerospace Tech

Author:

Nicolosi Fabrizio,Corcione Salvatore,Della Vecchia Pierluigi

Publisher

Emerald

Reference29 articles.

1. Design and Testing of a Multi-Element Airfoil for Short-Takeoff-and-Landing Ultralight Aircraft

2. Improving Hang-Glider Maneuverability Using Multiple Winglets: A Numerical and Experimental Investigation

3. Fink, M.P. and Freman, D.C., Jr (1969), “Full-scale wind-tunnel investigation of static longitudinal and lateral characteristics of a light twin-engine airplane”, NASA TN D-4983, National Aeronautics and Space Administration, Washington, DC.

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