| Citation: | TIAN Jin-hu, QIAO Wei-yang, PENG Sheng-hong. Calculation and analysis on air inlet/engine integrated in fast maneuvering flight[J]. Journal of Aerospace Power, 2013, 28(8): 1818-1827.
|
| [1] |
SAE S-16 Committee.ARP1420B gas turbine engine inlet flow distortion guidelines[M].Washington D C:Society of Automotive Engineers,2002.
|
| [2] |
Davis M,Baker W,Power G,et al.A proposal for integration of wind tunnel and engine test programs for the evaluation of air frame-propulsion compatibility using numerical simulations[J].Journal of Engineering for Gas Turbines and Power,2002,124(3):447-458.
|
| [3] |
Hale A,Davis M,Sirbaughet J,et al.A numerical simulation capability for analysis of aircraft inlet-engine compatibility[J].Journal of Engineering for Gas Turbines and Power,2006,128(3):473-481.
|
| [4] |
Haldeman C W,Dunn M G,Abhari R S,et al.Experimental and computational investigation of the time-averaged and time-resolved pressure loading on a waneless counter-rotating turbine [R].ASME Paper 2000-GT-0445,2000.
|
| [5] |
Beale D,O'Dowd K,Davis M,et al.An example for integrated gas turbine engine testing and analysis using modeling and simulation [R].Las Cruces:The 2006 ITEA Modeling and Simulation Conference,2006.
|
| [6] |
Davis M,Hale A.A parametric study on the effects of inlet swirl on compression system performance and operability using numerical simulations [R].ASME Paper GT-2007-27033,2007.
|
| [7] |
Beale D,Davis M,Sirbaugh J.Requirements and advances in simulating aircraft inlet total-pressure distortion in turbine engine ground tests [R].ASME Paper GT-2006-90038,2006.
|
| [8] |
Davis M.Parametric investigation into the combined effects of pressure and temperature distortion on compression system stability [R].AIAA 91-1895,1991.
|
| [9] |
Batterton P G,Gold H.Experimental test results of a generalized-parameter fuel control [R].NASA TN D-7198,1973.
|
| [10] |
Calogeras J E.Experimental investigation of dynamic distortion in a Mach 2.50 inlet with 60 percent internal contraction and its effect on turbojet stall margin [R].NASA TM X- 1842,1969.
|
| [11] |
Burstadt P L,Calogeras J E,Choby D A.Unstart and stall interactions between a turbojet engine and an axisymmetric inlet with 60-percent internal-area contraction [R].NASA TM X-2192,1971.
|
| [12] |
Hale A A, Davis M W, Sirbaugh J H. A numerical simulation capability for analysis of aircraft inlet-engine compatibility [R].ASME Paper 2004-GT-53473,2004.
|
| [13] |
Costakis W G,Wenzel L M.An experimental investigation of compressor stall using an on-line distortion indicator and signal conditioner [R].NASA TM X-3 182,1975.
|
| [14] |
Davis M W,Owen A K,O'Brien W F,et al.Joint dynamic airbreathing propulsion simulations partnership JDAPS [R].ASME Paper 95-GT-143 1995.
|
| [15] |
Garrard G D.ATEC:the aerodynamic turbine engine code for the analysis of transient and dynamic turbine engine system operations [D].Knoxville:The University of Tennessee,1995.
|
DownLoad: