J. F. Wasserbauer

发表

Performance and surge limits of a TF30-P-3 turbofan engine/axisymmetric mixed-compression inlet propulsion system at Mach 2.5

J. F. Wasserbauer, H. E. Neumann, R. J. Shaw, 1985 .

Dynamic response of a Mach 2.5 axisymmetric inlet with engine or cold pipe and utilizing 60 percent supersonic internal area contraction

J. F. Wasserbauer, 1969 .

Experimental and analytical investigation of the dynamic response of a supersonic mixed-compression inlet

J. F. Wasserbauer, R. G. Willoh, J. Wasserbauer, 1968 .

Inlet-engine matching for SCAR including application of a bicone variable geometry inlet. [Supersonic Cruise Aircraft Research]

J. F. Wasserbauer, W. H. Gerstenmaier, 1978 .

Low speed performance of a supersonic axisymmetric mixed compression inlet with auxiliary inlets. [Lewis 9x15-ft anechoic wind tunnel tests

J. F. Wasserbauer, C. J. Trefny, R. W. Cubbison, 1983 .

Supersonic cruise inlets

J. F. Wasserbauer, R. E. Coltrin, D. N. Bowditch, 1971 .

Minimizing boundary layer bleed for a mixed compression inlet. [sized for TF30-P-3 turbofan engine at Mach 2.0 and 2.5]

J. F. Wasserbauer, H. E. Neumann, R. J. Shaw, 1973 .

A 5-centimeter-diameter electron-bombardment thrustor with permanent magnets

J. F. Wasserbauer, 1966 .

Experimental investigation of the dynamic response of a supersonic inlet to external and internal disturbances

J. F. Wasserbauer, J. Wasserbauer, D. L. Whipple, 1968 .

Experimental mercury bombardment thruster at submillipound thrust.

W. R. Kerslake, J. F. Wasserbauer, P. M. Margosian, 1967 .

Performance of vortex generators in a Mach 2.5 low-bleed full scale 45-percent-internal-contraction axisymmetric inlet

J. F. Wasserbauer, H. E. Neumann, R. J. Shaw, 1975 .