Johnson, Forrester:
A General Panel Method for the Analysis and
Design of Arbitrary Configurations in Incompressible Flows.
NASA Contractor Report 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 Contractor Report 3062, 1979.
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. I. Theory Document (Version 1.0).
NASA Contractor Report 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 Contractor Report 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