Author:
Schuff Reuben,Jung Hogril,Merkle Charles,Anderson William
Publisher
American Institute of Aeronautics and Astronautics
Reference19 articles.
1. 2Wadel, M.F., and Meyer, M.L. "Validation of High Aspect Ratio Cooling in a 89 kN (20,000 Ibf) Thrust Combustion Chamber," AIAA-1996-2584, 32nd ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit, Lake Buena Vista, FL, 1996.
2. 3Carlile,J.andQuentmeyer,R."AnExperimentalInvestigationofHigh-Aspect-RatioCoolingPassages,"AIAA-1992-3154, SAE, ASME, and ASEE, JointPropulsion Conference and Exhibit,28th, Nashville, TN, July6-8,1992.
3. 5Taylor, M. F. "A Method of Predicting Heat Transfer Coefficients in the Cooling Passage of NERVA and PHOEBUS-2 Rocket Nozzles," NASA TM X-52437 AIAA-1968-608, 4th AIAA Propulsion Joint Specialist Conference, Cleveland, OH, June 10-14,1968.