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On the numerical simulation of three-dimensional transonic flow with application to the C-141 wing /
Published 1973CONNECT
Government Document Electronic eBook -
4
Effect of wing design on the longitudinal aerodynamic characteristics of a wing-body model at subsonic speeds /
Published 1972CONNECT
Government Document Electronic eBook -
5
Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation /
Published 1972CONNECT
Government Document Electronic eBook -
6
Theoretical span loading and moments of tapered wings produced by aileron deflection /
Published 1937CONNECT
Government Document Electronic eBook -
7
Full-scale span load distribution on a tapered wing with split flaps of various spans /
Published 1937CONNECT
Government Document Electronic eBook -
8
Wind-tunnel tests of a Clark Y wing with "Maxwell" leading-edge slots /
Published 1937CONNECT
Government Document Electronic eBook -
9
Full-scale wind-tunnel and flight tests of a Fairchild 22 airplane equipped with external-airfoil flaps /
Published 1937CONNECT
Government Document Electronic eBook -
10
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11
Empirical corrections to the span load distribution at the tip /
Published 1937CONNECT
Government Document Electronic eBook -
12
Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails.
Published 1937CONNECT
Government Document Electronic eBook -
13
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14
The effect of curvature on the transition from laminar to turbulent boundary layer /
Published 1937CONNECT
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15
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Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails.
Published 1937CONNECT
Government Document Electronic eBook -
17
Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails.
Published 1938CONNECT
Government Document Electronic eBook -
18
Interference of wing and fuselage from tests of eight combinations in the N.A.C.A. variable-density tunnel combinations with tapered fillets and straight-side junctures /
Published 1938CONNECT
Government Document Electronic eBook -
19
Interference of wing and fuselage from tests of 18 combinations in the N.A.C.A. variable-density tunnel combinations with split flaps /
Published 1938CONNECT
Government Document Electronic eBook -
20
Interference of wing and fuselage from tests of 17 combinations in the N.A.C.A. variable-density tunnel combinations with special junctures /
Published 1938CONNECT
Government Document Electronic eBook