References for the PanAir Program

User's Guides

• D6-54703, A502I User's Guide-PAN AIR Technology Program for Solving Potential Flow about Arbitrary Configurations, February 1992.

Theory

• Erickson, Larry L.: Panel Methods - An Introduction. NASA Technical Paper 2995, December 1990.
• Johnson, Forrester: A General Panel Method for the Analysis and Design of Arbitrary Configurations in Incompressible Flows, NASA CR 3079, May, 1980.

General Commentary

• Johnson, F. T. and Rubbert, P. E., "Advanced Panel-Type Influence Coefficient Methods Applied to Subsonic Flows," AIAA 75-50, January 1975.
• Ehlers, F. E., Johnson, F. T., and Rubbert, P. E., "A Higher Order Panel Method for Linearized Supersonic Flow." AIAA 76-381, July 1976.
• Ehlers, F. E., Epton, M. A., Johnson, F. T., Magnus, A. E., and Rubbert, P. E., "A Higher Order Panel Method for Linearized Supersonic Flow, NASA CR-3062, 1979.

PAN AIR Program

• Derbyshire, T. and Sidwell, K. W., "PAN AIR Summary Document, (Version 1.0)," NASA CR-3250, 1982.
• Magnus, A. E. and Epton, M. A., "PAN AIR-A Computer Program for Predicting Subsonic or Supersonic Linear Potential Flows About Arbitrary Configurations Using A Higher Order Panel Method," Vol. 1. Theory Document (Version 1.0), NASA CR-3251, 1980.
• Sidwell, K. W., Baruah, P. K., and Bussoletti, J. E., "PAN AIR-A Computer Program for Predicting Subsonic or Supersonic Linear Potential Flows About Arbitrary Configurations Using A Higher Order Panel Method, Vol. II. User's Manual (Version 1.0), NASA CR-3252, 1980.

Comparisons and Evaluations

• Thomas, J. L. and Miller, D. S., "Numerical Comparisons of Panel Methods at Subsonic and Supersonic Speeds," AIAA Paper 79-0404, January 1979.
• Sytsma, H. S., Hewill, B. L., and Rubbert, P. E., "A Comparison of Panel Methods for Subsonic Flow. Computation, AGARD Paper 241, May 1976.
• Thomas, J. L., Luckring, J. M., and Sellers M, W. L., "Evaluation of Factors Determining the Accuracy of Linearized Subsonic Panel Methods:, AIAA 83-1826.

Subsonic Applications

• Chen, A. W., and Tinoco, E. N., "PAN AIR Applications to Aero-Propulsion Integration", AIAA 83-1368, June 1983.
• Tinoco, E. N. and Chen, A. W., "CFD Applications to Engine/Airframe Integration," Numerical Methods for Engine-Airframe Integration, Vol. 102 of Progress in Astronautics and Aeronautics, AIAA, 1986.
• Wittenberg, K. R., Reichenbach, S. H, Kao, T. J., Tinoco, E. N., "CFD Wake and Flowfield Predictions," AIAA Paper 87-2618, August 1987.
• Miller, S. G., and Youngblood, D. B., "Applications of USSAERO-B and the PAN AIR Production Code to the CDAF Model A Canard/Wing Configuration," AIAA 83-1829, July 1983.
• Lee, K. D., "Numerical Simulation of the Wind Tunnel Environment by a Panel Method," AIAA 80-0419, March 1980.
• Snyder, L. D., and Erickson, L. L., "PAN AIR Prediction of NASA 12-Foot Pressure Wind Tunnel Interference on a Fighter Configuration" AIAA 84-0219, January 1984.
• Strande, S.; Erickson, L. L.; Snyder, L.D.; and Carmichael, R.L.: "PAN AIR Modeling Studies II: Sideslip Option, Network Gaps, Three-Dimensional Forebody Flow and Thick Trailing Edge Representation," AIAA 84-0220, January 1984.

Subsonic and Supersonic Applications

• Medan, R. T., Magnus, A. E., Sidwell, K. W., and Epton, M. A.: "PAN AIR-A Computer Program for Predicting Subsonic or Supersonic Linear Potential Flows About Arbitrary Configurations Using A Higher Order Panel Method, Vol. III, Case Manual (Version 1.0), NASA CR-3253,1981.
• Carmichael, R. L., and Erickson, L. L.: "PAN AIR - A Higher Order Panel Method for Predicting Subsonic or Supersonic Linear Potential Flows About Arbitrary Configurations," AIAA 81-1255, June 1981.
• Towne, M. C.; Strande, S. M.; Erickson, L. L.; Kroo, I. M.; Enomoto, F. Y.; Carmichael, R.L.; and McPherson, K. F.: "PAN AIR Modeling Studies," AIAA 83-1830, July 1983.

Supersonic Applications

• Tinoco, E. N., Johnson, F. T., and Freeman, L. M.: "The Application of a Higher Order Panel Method to Realistic Supersonic Configurations," AIAA 79-0247, January 1979.
• Cenko, A. and Tinoco, E. N.: "PAN AIR - Weapons Carriage and Separation," AFFDL-TR-79-3142, December 1979.
• Cenko, A., Tinoco, E. N., Dyer, R. K., and DeJongh, J.: "PAN AIR Applications to Weapons Carriage and Separation," AIAA 80-0187R, Journal of Aircraft, Vol. 18, No. 2, February 1981.
• Cenko, A., Tinoco, E. N., and Tustaniwskyj, J., "PAN AIR Applications to Mutual Interference Effects Due to Close Promixity," AIAA 84-0217, January 1984.
• Lamb, Milton, Sawyer, Wallace C., and Thomas, James L.: "Experimental and Theoretical Supersonic Lateral-Directional Stability Characteristics of a Simplified Wing-Body Configuration with a Series of Vertical-Tail Arrangements," NASA Technical Paper 1878, August 1981.
• Siclari, M., Visich, M., Cenko, A., Rosen, B., and Mason, W.: "An Evaluation of NCOREL, PAN AIR and W12SC3 for the Prediction of Pressures on a Supersonic Maneuver Wing," AIAA 84-0218, January 1984.
• Cenko, A., "PAN AIR Applications to Complex Configurations", AIAA-83-0007, Jan. 1983.

Boundary Layer Analysis

• Sullivan, Peter: User's Manual for the Viscous Panel Analysis System - Program A598, Boeing Commercial Airplanes, D6-54744, Seattle, WA, April 5,1989