Heat transfer and pressure on a flat plate and on protuberances in a supersonic turbulent boundary layer at mach 2.65, 3.51, and 4.4
Pressure and turbulent heat transfer associated with sinusoidal protuberances on flat plat
This experimental study documents the development and separation of a hypersonic boundary layer prod...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
Cover title."December 1962."Includes bibliographical references.Mode of access: Internet
Heat transfer measurements on flat plate with attached protuberances in turbulent boundary layer at ...
Local heat-transfer rates on the surface of a heated flat plate at zero incidence to an air stream f...
Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...
An experimental investigation was conducted in Leg 1 of the GALCIT 5 x 5 inch Hypersonic Wind Tunnel...
Heat transfer rates measured in front and to the side of a protrusion on an aluminum flat plate subj...
Heat transfer rates measured in front and to the side of a protrusion on an aluminum flat plate subj...
Flow field measurements on flat plate with attached protuberances in supersonic turbulent boundary l...
Heat transfer rate and pressure measurements were made upstream of surface pro-tuberances on a flat ...
The report presents a numerical study of attached interacting supersonic turbulent boundary layers o...
Conjugate heat transfer analysis of supersonic turbulent flow over a finite thickness flat plate is ...
SIGLELD:4360.17V(IC-AERO--82-04) / BLDSC - British Library Document Supply CentreGBUnited Kingdo
Pressure and turbulent heat transfer associated with sinusoidal protuberances on flat plat
This experimental study documents the development and separation of a hypersonic boundary layer prod...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
Cover title."December 1962."Includes bibliographical references.Mode of access: Internet
Heat transfer measurements on flat plate with attached protuberances in turbulent boundary layer at ...
Local heat-transfer rates on the surface of a heated flat plate at zero incidence to an air stream f...
Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...
An experimental investigation was conducted in Leg 1 of the GALCIT 5 x 5 inch Hypersonic Wind Tunnel...
Heat transfer rates measured in front and to the side of a protrusion on an aluminum flat plate subj...
Heat transfer rates measured in front and to the side of a protrusion on an aluminum flat plate subj...
Flow field measurements on flat plate with attached protuberances in supersonic turbulent boundary l...
Heat transfer rate and pressure measurements were made upstream of surface pro-tuberances on a flat ...
The report presents a numerical study of attached interacting supersonic turbulent boundary layers o...
Conjugate heat transfer analysis of supersonic turbulent flow over a finite thickness flat plate is ...
SIGLELD:4360.17V(IC-AERO--82-04) / BLDSC - British Library Document Supply CentreGBUnited Kingdo
Pressure and turbulent heat transfer associated with sinusoidal protuberances on flat plat
This experimental study documents the development and separation of a hypersonic boundary layer prod...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...