Theoretical and Experimental Results for the S414, Slotted, Natural-Laminar-Flow Airfoil-Reference-Cited by-同舟云学术

Theoretical and Experimental Results for the S414, Slotted, Natural-Laminar-Flow Airfoil

Published:2014-11 Issue:6 Volume:51 Page:1883-1890
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Coder James G.¹,Maughmer Mark D.¹,Somers Dan M.²

Affiliation:

1. Department of Aerospace Engineering, Pennsylvania State University, University Park, Pennsylvania 16802

2. Airfoils, Incorporated, Port Matilda, Pennsylvania 16870

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032566

Reference24 articles.

1. SomersD. M. “An Exploratory Investigation of a Slotted, Natural-Laminar-Flow Airfoil,” NASA CR-2012-217560, 2012.

2. WhitcombR. T.ClarkL. R. “An Airfoil Shape for Efficient Flight at Supercritical Mach Numbers,” NASA TM-X-1109, 1965.

3. SomersD. M.MaughmerM. D. “Design and Experimental Results for the S414 Airfoil,” U.S. Army Research, Development and Engineering Command TR-10-D-112, Aberdeen Proving Ground, MD, 2010.

4. SomersD. M.MaughmerM. D. “Design and Experimental Results for the S406 Airfoil,” U.S. Army Research, Development and Engineering Command TR-10-D-107, Aberdeen Proving Ground, MD, 2010.

5. SomersD. M.MaughmerM. D. “Design and Experimental Results for the S411 Airfoil,” U.S. Army Research, Development and Engineering Command TR-10-D-111, Aberdeen Proving Ground, MD, 2010.

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