Tomeki

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cowlings

1-7 of 7 Books

View The use of cowl camber and taper to reduce rotor/stator interaction noise By R. Martinez

The use of cowl camber and taper to reduce rotor/stator interaction noise

The use of cowl camber and taper to reduce rotor/stator interaction noise

By R. Martinez

View Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 By Scott Douglas Holland

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

By Scott Douglas Holland

View A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating By David M. McGowan

A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating

A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating

By David M. McGowan

View Viscous hypersonic shock-on-shock interaction on blunt cowl lips By Goetz H. Klopfer

Viscous hypersonic shock-on-shock interaction on blunt cowl lips

Viscous hypersonic shock-on-shock interaction on blunt cowl lips

By Goetz H. Klopfer

View Ultra high bypass nacelle areodynamics By Michael J. Larkin

Ultra high bypass nacelle areodynamics

Ultra high bypass nacelle areodynamics

By Michael J. Larkin

View Computational analysis in support of the SSTO flowpath test By Beverly S. Duncan

Computational analysis in support of the SSTO flowpath test

Computational analysis in support of the SSTO flowpath test

By Beverly S. Duncan

View Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 By Scott D. Holland

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

By Scott D. Holland