TECHNICAL PAPERS: Gas Turbines: Aircraft Engine

A Proposal for Integration of Wind Tunnel and Engine Test Programs for the Evaluation of Airframe-Propulsion Compatibility Using Numerical Simulations

[+] Author and Article Information
M. Davis, W. Baker, G. Power, D. Beale

Severdrup Technology, Inc., Arnold Engineering Development Center, AEDC, Arnold Air Force Base, TN 37389-9013

J. Eng. Gas Turbines Power 124(3), 447-458 (Jun 19, 2002) (12 pages) doi:10.1115/1.1391279 History: Received October 01, 1998; Revised March 01, 1999; Online June 19, 2002
Copyright © 2002 by ASME
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Smith, R. E., 1995, “Marrying Airframes and Engines in Ground Test Facilities—An Evolutionary Revolution,” AIAA Paper No. 95-0950.
SAE Aerospace Information Report, AIR-1419, 1983, “Inlet Total-Pressure Distortion Considerations for Gas Turbine Engines,” May.
SAE Aerospace Recommended Practice, ARP-1420, 1978, “Gas Turbine Engine Inlet Flow Distortion Guidelines,” Mar.
Robinson, C. E., Smith, G. D., and Matz, R. J., 1969, “Evaluation of an Ejector—Powered Engine Simulator at Transonic Mach Numbers,” Paper No. AEDC-TR-78-69.
Overall, B. W., 1972, “A Procedure for the Design of Complex Distortion Screen Patterns for Producing Specified Steady State Total-Pressure Profiles at the Inlet of Turbine Engines,” Paper No. AEDC-TR-72-10.
Overall, B. W., 1976, “Evaluation of an Airjet Distortion Generator Used to Produce Steady-State Total-Pressure Distortion at the Inlet of Turbine Engines,” Paper No. AEDC-TR-76-141.
Brimelow, B., Collins, T. P., and Pfefferkorn, G. A., 1976, “Engine Testing in a Dynamic Environment,” AIAA Paper No. 74-1198.
Lazalier, G. R., and Tate, J. T. “Development of a Prototype Discrete Frequency, Total-pressure Fluctuation Generator for Jet Engine/Inlet Compatibility Investigation,” Proceedings of the Air Force Airframe Propulsion Compatibility Symposium, June, Paper AFAPL-TR-69-103.
Reynolds, G. G., et al., 1973, “An Experimental Evaluation of Unsteady Flow Effects on an Axial Compressor—P3 Generator Program,” Paper No. AFAPL-TR-73-43.
Smith, C. F., and Podleski, S. D., 1994, “Installed F/A-18 Inlet Flow Calculations at 30 Degree Angle-of-Attack: A Comparative Study,” AIAA Paper No. 94-3213.
Power, G. D., Cooper, G. K., and Sirbaugh, J. R., 1995, “NPARC 2.2—Features and Capabilities,” AIAA Paper No. 95-2609.
Mayer, D. W., Anderson, B. H., and Johnson, T. A., 1998, “3D Subsonic Diffuser Design and Analysis,” AIAA Paper No. 98-3418.
Philhower, J. S., Robinson, D. E., and Brown, R. J., 1998, “Development of a Highly Offset Induction System for a Supersonic STOVL Fighter,” AIAA Paper No. 98-3417.
Chien,  K.-Y., 1982, “Predictions of Channel and Boundary-Layer Flows With at Low-Reynolds-Number Turbulence Model,” AIAA J., 20, No. 1, pp. 33–38.
Wilcox, D. C., 1992, “The Remarkable Ability of Turbulence Model Equations to Describe Transition,” Fifth Symposium on Numerical and Physical Aspects of Aerodynamic Flows, California State University, Long Beach, CA, Jan. 13–15.
Menter, F. R., 1993, Zonal Two Equation k-ω Turbulence Models for Aerodynamic Flows,” Paper No. AIAA-93-2906.
Spalart, P. R., and Allmaras, S. R., 1992, “A One-Equation Turbulence Model for Aerodynamic Flows,” AIAA Paper No. 92-0439.
Tramel, R. W., and Nichols, R. H., 1997, “A Highly-Efficient Numerical Method for Overset-Mesh Moving-Body Problems,” AIAA Paper No. 97-2040.
Nichols, R. H., 1991, “Calculation of the Flow in an Circular S-Duct Inlet,” Paper No. AIAA-91-0174.
Bush, R. H., Power, G. D., and Towne, C. E., 1998, “WIND: The Production Flow Solver of the NPARC Alliance,” AIAA Paper No. 98-0935.
Paynter,  G. C., 1997, “Response of a Two-Dimensional Cascade to an Upstream Disturbance,” AIAA J., 35, No. 3, pp. 434–440.
Paynter, G. C., Clark, L. T., and Cole, G. L., 1998, “Modeling the Response from a Cascade to an Upstream Acoustic Disturbance,” AIAA Paper No. 98-0953.
Hall, E. J., and Delaney, R. A., 1992, “Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task V—Unsteady Counterrotation Ducted Propfan Analysis, Final Report,” NASA CR 187126, NASA Contract NAS3-25270.
Adamczyk, J. J., 1985, “Model Equations for Simulating Flows in Multistage Turbomachinery,” ASME Paper No. 85-GT-226.
Hale,  A. A., and O’Brien,  W. F., 1998, “A Three-Dimensional Turbine Engine Analysis Compressor Code (TEACC) for Steady-State Inlet Distortion,” Journal of Turbomachinery ,120, pp. 422–430.
Hearsey, R. M., 1970, “HTO300—A Computer Program for the Design and Analysis of Axial turbomachinery,” Mar.
Garrard, D., Davis, M. W., Wehofer, S., and Cole, G., 1997, “A One-Dimensional, Time-Dependent Inlet/Engine Numerical Simulation for Aircraft Propulsion Systems,” ASME Paper No. 97-GT-333.
Numbers, K., and Hamed, A., 1997, “Development of a Coupled Inlet-Engine Dynamic Analysis Method,” AIAA Paper No. 97-2880.
Clark, L. T., 1995, “Dynamic Response Characteristics of a Mixed Compression Supersonic Inlet as Part of a Larger System,” AIAA Paper No. 95-0036.
Benek, J. A., and Kraft, E. M., 1998, “Validation Issues for Engine-Airframe Integration,” AIAA J., 36 , No. 5.


Grahic Jump Location
Current inlet-engine integration test methodology
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ARP-1420 surge margin definition
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Typical distortion screen and corresponding distortion pattern
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Schematic of airjet distortion generator
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Simulation of time variant distortion with steady-state patterns
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Inlet flow distortions at high angle of attack on F/A 18A
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Mach number in an S-duct inlet
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Axial pressure distribution—S-duct
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Overall TEACC methodology
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Schematic of current process for inlet testing and analysis
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Schematic of proposed improved process for inlet testing and analysis
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Schematic of current process for engine testing and analysis
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Schematic of envision improved process for engine testing and analysis
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Schematic of envisioned integrated test and evaluation for engine-inlet analysis




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