1-6 of 6 Books
Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber
Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber
By Mary F. Wadel
A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
By Kenneth J. Davidian
Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber
Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber
By Mary E. Wadel
Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles
Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles
By James R. Burley
The effect of cooling passage aspect ratio on curvature heat transfer enhancement
The effect of cooling passage aspect ratio on curvature heat transfer enhancement
By Michael L. Meyer
Electrically heated tube investigation of cooling channel geometry effects
Electrically heated tube investigation of cooling channel geometry effects
By Michael L. Meyer