...N. Sinha; J. Erwin; C. Kannepalli A practical framework for predicting jet structure and noise from military aircraft is described, which is developmental and has been examined for some fundamental jet flow problems. The framework currently utilizes Reynolds-averaged Navier Stokes (RANS...

... to 5.44% for the maneuvers analyzed. 12 04 2010 19 04 2010 12 11 2010 12 11 2010 aerospace propulsion aircraft testing boundary layers computational fluid dynamics cooling distortion jet engines mass transfer military aircraft nozzles supersonic flow thermal energy...

... turbine’s erosion upon the low-cycle fatigue life-consumption of aero-engine’s hot-end components) helps the users to take wiser management decisions. For a military aircraft’s mission profile, using bespoke computer simulations, the impacts of turbine erosion for high-pressure turbine-blade’s low-cycle...

... after expiration of the prescribed TBO. aerospace engines aerospace expert systems aircraft maintenance condition monitoring decision making fault tolerance inspection military aircraft remaining life assessment 22 11 2007 10 09 2008 29 01 2009 Turbine stator...

...-38760. Manuscript received by IGTI, October 2002, final revision, March 2003. Associate Editor: H. R. Simmons. 16 June 2003 01 October 2002 01 March 2003 15 04 2005 jet engines gas turbines cooling military aircraft Max Bentele was born on January 15, 1909...

... military aircraft aerospace engines aerospace propulsion rotation compressibility fuel product development There is an ongoing military need to fuel low-power (2–500 kW) small internal combustion engines with heavy diesel, or JP types of fuels. In that power range gas turbine engines have...

...David W. Milanes; Daniel R. Kirk; Krzysztof J. Fidkowski; Ian A. Waitz As commercial and military aircraft engines approach higher total temperatures and increasing overall fuel-to-air ratios, the potential for significant chemical reactions to occur downstream of the combustor is increased...

.... Manuscript received by IGTI, Dec. 2000, final revision, Mar. 2001. Associate Editor: R. Natole. 04 June 2001 01 Dec 2000 01 Mar 2001 27 12 2002 military aircraft aerospace engines aerospace propulsion detonation fuel drag reduction life cycle costing design engineering...

... Headquarters Jan. 2001. Associate Editor: M. Magnolet. 08 May 2000 01 Feb 2000 01 Jan 2001 24 09 2002 gas turbines Mach number controllers fuel military aircraft Toyne, G. B., and Hodges, G. S., 1983, “All-Electric Accessory Drive Systems: Implications on Engine...

... by ASME Headquarters Jan. 2001. Associate Editor: M. Magnolet. 08 May 2000 01 Feb 2000 01 Jan 2001 military aircraft engines design for testability mechanical engineering Unmanned air vehicles are in military operation today, designed primarily for reconnaissance...