| Raman measurement of mixing and finite-rate chemistry in a supersonic hydrogen-air diffusion flame TS Cheng, JA Wehrmeyer, RW Pitz, O Jarrett Jr, GB Northam Combustion and Flame 99 (1), 157-173, 1994 | 200 | 1994 |
| Survey of supersonic combustion ramjet research at Langley G Northam, G Anderson 24th Aerospace Sciences Meeting, 159, 1986 | 117 | 1986 |
| Plasma torch igniter for scramjets TC Wagner, WF O'Brien, GB Northam, JM Eggers Journal of Propulsion and Power 5 (5), 548-554, 1989 | 106 | 1989 |
| Evaluation of parallel injector configurations for supersonic combustion G Northam, I Greenberg, C Byington 25th joint propulsion conference, 2525, 1989 | 97 | 1989 |
| Application of absorption filter planar Doppler velocimetry to sonic and supersonic jets MW Smith, GB Northam, JP Drummond AIAA journal 34 (3), 434-441, 1996 | 80 | 1996 |
| Effects of hydrogen active cooling on scramjet engine performance Y Tsujikawa, GB Northam International Journal of Hydrogen Energy 21 (4), 299-304, 1996 | 74 | 1996 |
| Velocity and thermal structure, and strain-induced extinction of 14 to 100% hydrogen-air counterflow diffusion flames GL Pellett, KM Isaac, WM Humphreys Jr, LR Gartrell, WL Roberts, ... Combustion and Flame 112 (4), 575-592, 1998 | 66 | 1998 |
| Evaluation of parallel injector configurations for Mach 2 combustion GB Northam, I Greenberg, CS Byington, DP Capriotti Journal of Propulsion and Power 8 (2), 491-499, 1992 | 58 | 1992 |
| Development and evaluation of a plasma jet flameholder for scramjets G Northam, C McClinton, W Obrien 20th Joint Propulsion Conference, 1408, 1984 | 51 | 1984 |
| Study of a supersonic combustor employing swept ramp fuel injectors DR Eklund, SD Stouffer, GB Northam Journal of Propulsion and Power 13 (6), 697-704, 1997 | 46 | 1997 |
| Effects of scale on supersonic combustor performance G DISKIN, G Northam 23rd Joint Propulsion Conference, 2164, 1987 | 46 | 1987 |
| Finite-rate chemistry effects in a Mach 2 reacting flow T Cheng, J Wehrmeyer, R Pitz, O JARRETT, JR, G Northam 27th Joint Propulsion Conference, 2320, 1991 | 41 | 1991 |
| Dustsonde and lidar measurements of stratospheric aerosols: A comparison GB Northam, JM Rosen, SH Melfi, TJ Pepin, MP McCormick, DJ Hofmann, ... Applied Optics 13 (10), 2416-2421, 1974 | 39 | 1974 |
| Numerical predictions of a rearward-facing-step flow in a supersoniccombustor K Uenishi, RC Rogers, GB Northam Journal of Propulsion and Power 5 (2), 158-164, 1989 | 35 | 1989 |
| Effects of compression and expansion ramp fuel injector configuration on scramjet combustion and heat transfer SD Stouffer, NR Baker, DP Capriotti, GB Northam AIAA, Aerospace Sciences Meeting and Exhibit, 1993 | 34 | 1993 |
| Coherent anti-Stokes Raman spectroscopy temperature measurements in a hydrogen-fueled supersonic combustor MW Smith, O Jarrett Jr, RR Antcliff, GB Northam, AD Cutler, DJ Taylor Journal of Propulsion and Power 9 (2), 163-168, 1993 | 33 | 1993 |
| Three-dimensional computations of transverse hydrogen jet combustionin a supersonic airstream K Uenishi, R Rogers, G Northam 25th AIAA Aerospace Sciences Meeting, 89, 1987 | 30 | 1987 |
| Effects of acceleration upon solid-rocket performance. GB Northam, MH Lucy Journal of Spacecraft and Rockets 6 (4), 456-459, 1969 | 29 | 1969 |
| Computational/experimental investigation of staged injection into a Mach 2 flow DR Eklund, DG Fletcher, RJ Hartfield Jr, JC McDaniel, GB Northam, ... AIAA journal 32 (5), 907-916, 1994 | 25 | 1994 |
| Mach 2 and Mach 3 mixing and combustion in scramjets GB Northam, DP Capriotti, CS Byington, I Greenberg | 25 | 1991 |
