B. K. Hodder

发表

An investigation of engine influence on inlet performance. [conducted in the Ames 40- by 80-foot wind tunnel

B. K. Hodder, 1981 .

Further studies of static to flight effects on fan tone noise using inlet distortion control for source identification

B. K. Hodder, 1976 .

Investigation of the effect of inlet turbulence length scale on fan discrete tone noise

B. K. Hodder, 1973 .

Aerodynamic characteristics of a large-scale model with a lift fan mounted in a 5 per cent thick triangular wing, including the effects of BLC on the lift fan inlet

B. K. Hodder, J. V. Kirk, L. P. Hall, 1970 .

Aerodynamic characteristics of a large-scale V/STOL transport model with tandem lift fans mounted at mid-semispan of the wing

B. K. Hodder, S. O. Dickinson, L. P. Hall, 1971 .

The effects of forward speed on fan inlet turbulence and its relation to tone noise generation

B. K. Hodder, 1974 .

Aerodynamics of lift fan V/STOL aircraft

B. K. Hodder, J. V. Kirk, L. P. Hall, 1971 .

A large-scale investigation of engine influence on inlet performance at angle-of-attack

B. K. Hodder, B. W. Farquhar, M. R. Dudley, 1981 .

Large-scale wind-tunnel investigation of a V/STOL transport model with wing-mounted lift fans and fuselage-mounted lift-cruise engines for propulsion

B. K. Hodder, J. V. Kirk, L. P. Hall, 1967 .