1. Gas turbine combustion;Lefebvre,1983
2. Aircraft turbine engine combustors—development status/challenges;Bahr,1989
3. Segalman I, McKinney RG, Sturgess GJ, Huang L-M. Reduction of NOx by fuel-staging in gas turbine engines—a commitment to the future. AGARD Conference Proceedings 536, 1993. p. 29/1–17.
4. Modification of combustor stoichiometry distribution for reduced NOx emission from aircraft engines;Sturgess;Trans ASME,1983
5. Corbett NC, Lines NP. Control requirements for the RB 211 low emission combustion system, ASME International Gas Turbine and Aeroengine Congress and Exposition, Cincinnati, OH, paper 93-GT-12, 1993.