PDAS home > Contents > PanAir > Panair Refs
Public Domain Aeronautical Software (PDAS)  

User's Guides

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

Theory

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

General Commentary

  1. Johnson, F. T. and Rubbert, P. E., "Advanced Panel-Type Influence Coefficient Methods Applied to Subsonic Flows," AIAA 75-50, January 1975.
  2. Ehlers, F. E., Johnson, F. T., and Rubbert, P. E., "A Higher Order Panel Method for Linearized Supersonic Flow." AIAA 76-381, July 1976.
  3. 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

  1. 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.

Comparisons and Evaluations

  1. Thomas, J. L. and Miller, D. S., "Numerical Comparisons of Panel Methods at Subsonic and Supersonic Speeds," AIAA Paper 79-0404, January 1979.
  2. Sytsma, H. S., Hewill, B. L., and Rubbert, P. E., "A Comparison of Panel Methods for Subsonic Flow. Computation, AGARD Paper 241, May 1976.
  3. 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

  1. Chen, A. W., and Tinoco, E. N., "PAN AIR Applications to Aero-Propulsion Integration", AIAA 83-1368, June 1983.
  2. 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.
  3. Wittenberg, K. R., Reichenbach, S. H, Kao, T. J., Tinoco, E. N., "CFD Wake and Flowfield Predictions," AIAA Paper 87-2618, August 1987.
  4. 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.
  5. Lee, K. D., "Numerical Simulation of the Wind Tunnel Environment by a Panel Method," AIAA 80-0419, March 1980.
  6. 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.
  7. 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

  1. 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.
  2. 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.
  3. 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

  1. 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.
  2. Cenko, A. and Tinoco, E. N., "PAN AIR - Weapons Carriage and Separation," AFFDL-TR-79-3142, December 1979.
  3. Cenko, A., Tinoco, E. N., Dyer, R. K., and DeJongh, J., "PAN AIR Applications to Weapons Carriage and Separation," AIAA 80-0187R, J. Aircraft, Vol. 18, No. 2, February 1981.
  4. Cenko, A., Tinoco, E. N., and Tustaniwskyj, J., "PAN AIR Applications to Mutual Interference Effects Due to Close Promixity," AIAA 84-0217, January 1984.
  5. 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.
  6. 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.
  7. Cenko, A., "PAN AIR Applications to Complex Configurations", AIAA-83-0007, Jan. 1983.

Boundary Layer Analysis

  1. Sullivan, Peter, User's Manual for the Viscous Panel Analysis System - Program A598, Boeing Commercial Airplanes, D6-54744, Seattle, WA, April 5,1989
PDAS home > Contents > PanAir > Panair Refs
Public Domain Aeronautical Software (PDAS)