J. N. Nielsen

发表

The equivalent angle-of-attack method for estimating the nonlinear aerodynamic characteristics of missile wings and control surfaces

M. J. Hemsch, J. N. Nielsen, 1982 .

Prediction of Aerodynamic Characteristics of Cruciform Missiles to High Angles of Attack Utilizing a Distributed Vortex Wake.

C. A. Smith, J. N. Nielsen, 1979 .

Aerodynamic characteristics of missile control fins in nonlinear flow fields

M. J. Hemsch, J. N. Nielsen, 1983 .

Equivalent angle-of-attack method for estimating nonlinear aerodynamics of missile fins

M. J. Hemsch, J. N. Nielsen, 1983 .

Influence of Support Systems on the Aerodynamics of an Inclined Ogive Cylinder

J. N. Nielsen, T. N. Canning, 1982 .

THEORETICAL AERODYNAMICS OF FLEXIBLE WINGS AT LOW SPEEDS. III, APPROXIMATE RESULTS FOR WINGS OF LARGE ASPECT RATIO,

J. N. Nielsen, A. R. Kriebel, 1964 .

Supersonic wing-body inteference at high angles of attack with emphasis on low aspect ratios

J. N. Nielsen, 1986 .

Computer programs for calculating pressure distributions including vortex effects on supersonic monoplane or cruciform wing-body-tail combinations with round or elliptical bodies

M. F. E. Dillenius, J. N. Nielsen, 1979 .

New methods in engineering education

J. N. Nielsen, 1980 .

The equivalent angle-of-attack concept for engineering analysis

M. J. Hemsch, J. N. Nielsen, 1986 .

Circulation control airfoils - Past, present, future

N. J. Wood, J. N. Nielsen, N. Wood, 1985 .

Extension of equivalent angle-of-attack method for nonlinear flowfields

M. J. Hemsch, J. N. Nielsen, 1985 .

Theory of Flexible Aerodynamic Surfaces

J. N. Nielsen, J. Nielsen, 1963 .