Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds / by Bernard N. Daley and Douglas R. Lord.
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Other title: | Aerodynamic characteristics of several six-percent-thick airfoils at angles of attack from zero degrees to twenty degrees at high subsonic speeds. |
Format: | Government Document eBook |
Language: | English |
Published: |
Washington, [D.C.] :
National Advisory Committee for Aeronautics,
1955.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3424. |
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Internet
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Call Number: |
Y 3.N 21/5:6/3424
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Y 3.N 21/5:6/3424 | Available |