1 |
Uselton, B. L., "A Description of the Standard Dynamic Model(SDM)," 56th Supersonic Tunnel Association Meeting.
|
2 |
Roe, R. L., "Approximate Riemann Solvers, Parameter Vector and Difference Scheme," Journal. of Computational Physics, Vol. 43, No. 2, 1981, pp.357.
DOI
ScienceOn
|
3 |
Van Leer, B., "Towards the Ultimate Conservative Difference Scheme. V. A Second Order Sequel to Godunov's Method," Journal of Computational Physics, Vol. 32, 1979, pp.101-136.
DOI
ScienceOn
|
4 |
Beam, R. M. and Warming, R. F., "Implicit Numerical Methods for the Compressible Navier Stokes and Euler Equations," von Karman Institute for Fluid Dynamics Lecture Series, 1982-04, 1982.
|
5 |
Nicolaides, J. D., and Bolz, R. E., "On the Pure Rolling Motion of Winged and/or Finned Missiles in Varying Supersonic Flight," J. Aeronaut, Sci., Vol. 8, pp. 160-168, 1953.
|
6 |
Michael, E. B., "Determination of Static and Dynamic Stability Coefficients using Beggar," Master Thesis, Air Force Institute of Technology, Ohio, 2008.
|
7 |
Shantz, I. and Graves, R. T., "Dynamic and Static Stability Measurements of the Basic Finner at Supersonic Speeds." NAVORD Report 4516, Sept, 1960.
|
8 |
MacAllister, L. C., "The Aerodynamic Properties of a Simple Non-Rolling Finned Cone-Cylinder Configuration Between Mach number 1.0 and 2.5," BRL Report No. 934, 1955.
|
9 |
Oktay, E. and Akaym H. U., "CFD Prediction of Dynamic Derivatives For Missiles," 40th AIAA Aerospace Sciences Meeting, Reno, NV, 2002.
|
10 |
Murthy, H. S., "Subsonic and Transonic Roll Damping Measurements on Basic Finner," AIAA paper 82-4042, 1982.
|
11 |
Moore, F. G. and Swanson, R. C., "Dynamic Derivatives for Missile Configurations to Mach Number Three," Journal of Spacecraft and Rockets, Vol. 15, No. 2, pp. 65-66, 1978.
DOI
ScienceOn
|
12 |
Huang, X. Z., "Wing and Fin Buffet on The Standard Dynamic Model," NATO RTO Report Number RTO-TR-26, pp. 361-381, 1981.
|
13 |
Beyers, M. E., "Direct Derivative Measurements in the Presence of Sting Plunging," AIAA Paper 84-2107, 1984.
|
14 |
Fred, B. C., "Sting Interference Effects on the Static Dynamic, and Base Pressure Measurements of the Standard Dynamics Model Aircraft at Mach Numbers 0.3 through 1.3," AEDC-TR-81-3, 1981.
|
15 |
Winchenbach, G. L., Uselton, B. L., Hathaway, W. H., and Chelekis, R. M., "Comparison of Free-Flight and Wind Tunnel Data for a Generic Fighter Configuration," AIAA Paper 82-1365, 1982.
|
16 |
Murman, S. M., "A Reduced-Frequency Approach for Calculating Dynamic Derivatives," 43th AIAA Aerospace Science Meeting, Reno, NV, 2005.
|
17 |
Ronch, A. D., Vallespin, D., Ghoreyshi, and Badcock, K. J., "Computation of Dynamic Derivatives Using CFD," 28th AIAA Applied Aerodynamics Conference, 2010.
|
18 |
Merkle, C. L. and Athavale, M., "Time-Accurate Unsteady Incompressible Flow Algorithms Based on Artificial Compressibility," AIAA Paper 87-1137, Proceedings of AIAA 8th Computational Fluid Dynamics Conferenece, Honolulu, Hawaii, 1987.
|
19 |
Sturek, W. B., Nietubicz, C. J., Sahu, J., and Weinacht, P., "Applications of Computational Fluid Dynamics to the Aerodynamics of Army Projectiles," Journal of Spacecraft and Rockets, Vol. 31, No. 2, 1994, pp. 186-199.
DOI
ScienceOn
|
20 |
Newman, D. M., "Measurement of Water Tunnel Model Dynamic Derivatives using a Force Balance Capable of Rotational Oscillation," Contractor Report 2005.003, V0.20, Quantitative Aeronautics, 2006.
|
21 |
Limache, A.C., "Aerodynamic Modeling Using Computational Fluid Dynamics and Sensitivity Equations," Ph.D Thesis, Virginia Polytechnic Institute and State University, Blacksburg, 2000.
|
22 |
Wiess, J. M. and Smith, W. A., "Preconditioning Applied to Variable and Constant Density Flows," AIAA Journal, Vol. 32, No. 11, 1995, pp. 2050-2057.
|
23 |
Bryan, G. H., "Stability in Aviation," MacMillan, London, 1911.
|
24 |
Williams, J. E. and Vukelich, S. R., "USAF Stability and Control DATCOM," 1979.
|
25 |
Murphy, C. H., "Free Flight Motion of Symmetric Missiles," U.S. Army BRL, Report No. 1216, 1963.
|
26 |
Tobak, M. and Schiff, L. B., "Generalized Formulation of Nonlinear Pitch-Yaw-Roll Coupling," AIAA Journal, Vol. 13, No. 3, pp.323-332, 1975.
DOI
ScienceOn
|
27 |
Weinacht, P., "Navier-Stokes Predictions of the Individual Components of the Pitch-Damping Sum," Journal of Spacecraft and Rockets, Vol. 35, No. 5, pp. 598-605, 1998.
DOI
ScienceOn
|
28 |
Park, S. H., Kim, Y., Kwon, J. H., "Prediction of Dynamic Damping Coefficients Using Unsteady Dual-Time Stepping Method," 40th AIAA Aerospace Sciences Meeting, Reno, NV, 2002.
|
29 |
Green, L., Spence, A. M., and Murphy, P. C., "Computational Methods for Dynamic Stability and Control Derivatives," AIAA Papers 2004-0015, 2004.
|
30 |
Park, M. A. and Green L., "Steady-State Computation of Constant Rotational Rate Dynamic Stability Derivatives," 18th AIAA Applied Aerodynamics Conference, Denver, Colorado, 2000.
|