J. F. Schmidt

Performance with and without inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region

J. F. Schmidt, Robert S. Ruggeri · NASA STI Repository (National Aeronautics and Space Administration) · 1978 · 27 citations · Full text

Aeroacoustics, Engineering, Aerospace Engineering +10

Design and Performance of Controlled-Diffusion Stator Compared with Original Double-Circular-Arc Stator

T. F. Gelder, J. F. Schmidt, Kenneth L. Suder et al. · SAE technical papers on CD-ROM/SAE technical paper series · 1987 · 23 citations · Full text

Supersonic through-flow fan design

J. F. Schmidt, R. D. Moore, J. R. Wood et al. · 23rd Joint Propulsion Conference · 1987 · 20 citations · Full text

Unsteady Flow, Supersonic Through-flow Fan, Compressible Flow +10

Effect of Uncooled Inlet Length and Nozzle Convergence Angle on the Turbulent Boundary Layer and Heat Transfer in Conical Nozzles Operating With Air

D. R. Boldman, J. F. Schmidt, R. C. Ehlers · Journal of Heat Transfer · 1967 · 20 citations

Engineering, Fluid Mechanics, Turbulent Boundary Layer +16

Laminarization of a turbulent boundary layer as observed from heat-transfer and boundary layer measurements in conical nozzles

D. R. Boldman, Anthony Gallagher, J. F. Schmidt · NASA Technical Reports Server (NASA) · 1968 · 18 citations · Full text

Unsteady Flow, Boundary Layer Measurements, Engineering +11