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161
The effects of partial-span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y-wing /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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162
Tests of N-85, N-86, and N-87 airfoil sections in the 11-inch high-speed wind tunnel /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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163
Experimental study of deformation and of effective width in axially loaded sheet-stringer panels /
Published 1939“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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164
A method of rapidly estimating the position of the laminar separation point /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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165
Flow observations with tufts and lampblack of the stalling of four typical airfoil sections in the N.A.C.A. variable-density tunnel /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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166
The pressure available for ground cooling in front of the cowling of air-cooled airplane engines /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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Government Document Electronic eBook -
167
Scavenging a piston-ported two-stroke cylinder /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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Government Document Electronic eBook -
168
The charging process in a high-speed, single-cylinder, four-stroke engine /
Published 1939“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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169
Discharge characteristics of a simulated unit injection system /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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Government Document Electronic eBook -
170
Tests of a contra-propeller for aircraft /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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171
Hydrodynamic and aerodynamic tests of four models of outboard floats (N.A.C.A. Models 51-A, 51-B, 51-C, and 51-D) /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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172
Comparative performance of engines using a carburetor, manifold injection, and cylinder injection /
Published 1939“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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173
A general tank test of a model of the hull of the P3M-1 flying boat including a special working chart for the determination of hull performance /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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174
The unsteady lift of a finite wing /
Published 1939“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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Government Document Electronic eBook -
175
Pressure-distribution measurements on a tapered wing with a full-span split flap in curved flight /
Published 1939“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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Government Document Electronic eBook -
176
Circulation measurements about the tip of an airfoil during flight through a gust /
Published 1939“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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177
Local instability of symmetrical rectangular tubes under axial compression /
Published 1939“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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178
Loads imposed on intermediate frames of stiffened shells /
Published 1939“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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179
Longitudinal stability in relation to the use of an automatic pilot /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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Government Document Electronic eBook -
180
Operational treatment of the nonuniform-lift theory in airplane dynamics /
Published 1938“…Technical note (United States. National Advisory Committee for Aeronautics) ;…”
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