Fred R. DeJarnette
Affiliations: | North Carolina State University, Raleigh, NC |
Area:
Aerospace EngineeringGoogle:
"Fred DeJarnette"Children
Sign in to add trainee| Karen E. Harwell | grad student | 2000 | NCSU |
| Artem A. Dyakonov | grad student | 2010 | NCSU |
BETA: Related publications
See more...
Publications
|
You can help our author matching system! If you notice any publications incorrectly attributed to this author, please sign in and mark matches as correct or incorrect. |
| Hamilton HH, Weilmuenster KJ, DeJarnette FR. (2014) Approximate method for computing convective heating on hypersonic vehicles using unstructured grids Journal of Spacecraft and Rockets. 51: 1288-1305 |
| Lohmeyer WQ, DeJarnette FR. (2012) Transition from Laminar to Turbulent Boundary Layers Journal of Spacecraft and Rockets. 49: 766-768 |
| DeJarnette FR, Radcliffe RA. (1996) Matching inviscid/boundary-layer flowfields Aiaa Journal. 34: 35-42 |
| Riley CJ, DeJarnette FR. (1995) Engineering interactive inviscid boundary-layer method for hypersonic flow Journal of Spacecraft and Rockets. 32: 1081-1083 |
| Cheatwood FM, DeJarnette FR. (1994) Approximate viscous shock layer technique for calculating hypersonic flows around blunt-nosed bodies Journal of Spacecraft and Rockets. 31: 621-629 |
| Hamilton HH, Greene FA, Dejarnette FR. (1994) Approximate method for calculating heating rates on three-dimensional vehicles Journal of Spacecraft and Rockets. 31: 345-354 |
| Moore FG, Armistead MJ, Rowles SH, et al. (1993) New Approximate Method for Calculating Real Gas Effects on Missile Configurations Journal of Spacecraft and Rockets. 30: 22-31 |
| Hassan B, Dejarnette FR, Zoby EV. (1993) Effect of Nose Shape on Three-Dimensional Streamlines and Heating Rates Journal of Spacecraft and Rockets. 30: 69-78 |
| Landrum DB, Dejarnette FR, Boman BL. (1992) Engineering Method for Calculating Surface Pressures and Heating Rates on Vehicles with Embedded Shocks Journal of Spacecraft and Rockets. 29: 756-764 |
| Riley CJ, Dejarnette FR. (1991) Engineering calculations of three-dimensional inviscid hypersonic flowfields Journal of Spacecraft and Rockets. 28: 628-635 |