1-12 of 12 Books
Cavity unsteady-pressure measurements at subsonic and transonic speeds
Cavity unsteady-pressure measurements at subsonic and transonic speeds
By Maureen B. Tracy
Calculation of three-dimensional (3-D) internal flow by means of the velocity-vorticity formulation on a staggered grid
Calculation of three-dimensional (3-D) internal flow by means of the velocity-vorticity formulation on a staggered grid
By Paul M. Stremel
Three-dimensional cavity flow fields at subsonic and transonic speeds
Three-dimensional cavity flow fields at subsonic and transonic speeds
By Elizabeth B. Plentovich
Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
By A. B. Blair
Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization
Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization
By Oktay Baysal
A numerical study of laminar, incompressible, recirculation flows in rectangular and cylindrical cavities
A numerical study of laminar, incompressible, recirculation flows in rectangular and cylindrical cavities
By Daniel Y. Yamane
Experimental cavity pressure measurements at subsonic and transonic speeds
Experimental cavity pressure measurements at subsonic and transonic speeds
By Elizabeth B. Plentovich
Aeropropulsion technology (APT)
Aeropropulsion technology (APT)
By N. J. Heidegger
Parallelization of a multigrid incompressible viscous cavity flow solver using openMP
Parallelization of a multigrid incompressible viscous cavity flow solver using openMP
By Kevin Roe
Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes
Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes
By K. K. Ahuja
Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aeroacoustic codes
Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aeroacoustic codes
By K. K. Ahuja
Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By Maureen B. Tracy