Quasisteady aerodynamics for flutter analysis using steady computational fluid dynamics calculations

Journal of Aircraft

Volumn 33, Issue 1, 1996, Pages 191-197

  Scott, Robert C ^a,c   Pototzky, Anthony S ^b,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b LOCKHEED MARTIN   (United States)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; PRESSURE MEASUREMENT;

QUASISTEADY AERODYNAMICS;

FLUTTER (AERODYNAMICS);

EID: 0029696941     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.46921     Document Type: Article

References (5)

1. Ashley, H., and Zartarian, G., "Theoretical Hypervelocity Unsteady Aerodynamics," Proceedings of Symposium on Aerothermoelasticity, USAF ASD TR 61-645, Wright-Patterson AFB, OH, 1961, pp. 161-218.
2. Wagner, R. D., "Some Aspects of the Modified Newtonian and Prandtl-Meyer-Expansion Method for Axisymmetric Blunt Bodies," Ph.D. Dissertation, Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, Cambridge, MA, June 1961.
3. Walters, R., Reu, T., McGrory, W., Thomas, J., and Richardson, P., "A Longitudinally-Patched Grid Approach with Applications to High Speed Flows," AIAA Paper 88-0715, Jan. 1988.
4. Etkin, B. Z., Dynamics of Flight, Wiley, New York, 1982, pp. 137-140.
5. Peele, E. L., and Adams, W. M., "A Digital Program for Calculating the Interactions Between Flexible Structures, Unsteady Aerodynamics and Active Controls," NASA TM-80040, Jan. 1989.