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WInd-tunnel tests of ailerons at various speeds. : 4 - Ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt-nose balance on the NACA 23012 airfoil... by Letko, W.
Published 1943Call Number: Loading…
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2
Wind-tunnel tests of ailerons at various speeds. : 3 - Ailerons of 0.20 airfoil chord and true contour with 0.35-aileron-chord Frise balance on the NACA 23012 airfoil / by Letko, W.
Published 1943Call Number: Loading…
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3
WInd-tunnel tests of ailerons at various speeds. : 1 - Ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt nose balance on the NACA 66,2-216 airfo... by Letko, W.
Published 1943Call Number: Loading…
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4
WInd-tunnel tests of ailerons at various speeds. : 5 - Pressure distributions over the NACA 66,2-216 and NACA 23012 airfoils with various balances on 0.20-chord ailerons / by Letko, W.
Published 1943Call Number: Loading…
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5
The effect of cowling shape on the stability characteristics of an airplane / by Donlan, C. J.
Published 1942Other Authors: “…Letko, W.…”
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