Drag, heat transfer, and number flux were measured on sharp cones in the near free, molecule flow regime, and the results were compared with available Monte Carlo calculations. In general, the calculations predicted the magnitude of the data; however, the heat transfer and drag increased with increasing Knudsen number at a faster rate than predicted. Also the drag coefficients measured for the slender cones at high Knudsen number were higher than predicted for free molecule flow. These disagreements between theory and experiment could possibly be attributed to the simplicity of the surface interaction laws assumed in the theory. Reynolds analogy factors obtained from the experimental measurements agreed with free-molecule values and also wi...
Boundary-layer-transition and heat-transfer measurements were obtained from flight tests of blunt an...
Accurate simulation and modeling the effects of rarefaction on heat and mass transport is of much in...
Convective heat transfer rates on large angle conical bodies at hypersonic speed
Drag, heat transfer, and number flux were measured on sharp cones in the near free, molecule flow re...
The drag coefficients for cones with hot and cold walls and different bluntness ratios have been fou...
Various parameters have been suggested as correlation parameters for high-speed rarefied flow, or as...
Numerical results obtained with the direct simulation Monte Carlo (DSMC) method are presented for Ma...
Hypersonic transitional flow has been studied using the Direct Simulation Monte Carlo method. The cy...
Results of a numerical study are presented for hypersonic low-density flow about a 70-deg blunt cone...
Shock-dominated hypersonic laminar flows over a double cone are investigated using time accurate dir...
High Mach number wind tunnel drag, lift, moment, and heat-transfer data from sting-mounted models ar...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76131/1/AIAA-2001-2900-632.pd
Abstract. Various parameters have been suggested as correlation parameters for high-speed rarefied f...
Results of a numerical study concerning flow past a 70-deg blunted cone in hypersonic low-density fl...
Tests at M = 8.2 show that a simulated rocket plume at the base of a blunted cone can cause large ar...
Boundary-layer-transition and heat-transfer measurements were obtained from flight tests of blunt an...
Accurate simulation and modeling the effects of rarefaction on heat and mass transport is of much in...
Convective heat transfer rates on large angle conical bodies at hypersonic speed
Drag, heat transfer, and number flux were measured on sharp cones in the near free, molecule flow re...
The drag coefficients for cones with hot and cold walls and different bluntness ratios have been fou...
Various parameters have been suggested as correlation parameters for high-speed rarefied flow, or as...
Numerical results obtained with the direct simulation Monte Carlo (DSMC) method are presented for Ma...
Hypersonic transitional flow has been studied using the Direct Simulation Monte Carlo method. The cy...
Results of a numerical study are presented for hypersonic low-density flow about a 70-deg blunt cone...
Shock-dominated hypersonic laminar flows over a double cone are investigated using time accurate dir...
High Mach number wind tunnel drag, lift, moment, and heat-transfer data from sting-mounted models ar...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76131/1/AIAA-2001-2900-632.pd
Abstract. Various parameters have been suggested as correlation parameters for high-speed rarefied f...
Results of a numerical study concerning flow past a 70-deg blunted cone in hypersonic low-density fl...
Tests at M = 8.2 show that a simulated rocket plume at the base of a blunted cone can cause large ar...
Boundary-layer-transition and heat-transfer measurements were obtained from flight tests of blunt an...
Accurate simulation and modeling the effects of rarefaction on heat and mass transport is of much in...
Convective heat transfer rates on large angle conical bodies at hypersonic speed