FASTOP: A flutter and strength optimization program for lifting-surface structures

Journal of Aircraft

Volumn 14, Issue 6, 1977, Pages 581-587

  Wilkinson, Keith ^a   Markowitz, Joel ^a   Lerner, Edwin ^a   George, Dino ^a   Batill, Stephen M ^b  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

STRUCTURAL DESIGN - OPTIMIZATION;

AERODYNAMICS;

EID: 0017503106     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.58824     Document Type: Article

References (5)

1. Wilkinson, K., Markowitz, J., Lerner, E., Chipman, R., George, D., et al, “An Automated Procedure for Flutter and Strength Analysis and Optimization of Aerospace Vehicles, Vol. I-Theory, Vol. II-ProgramUsers Manual,” AFFDL-TR-75-137, Dec. 1975.
2. Dwyer, W. J., Emerton, R., and Ojalvo, I., “An Automated Procedure for the Optimization of Practical Aerospace Structures, Vol. I - Theoretical Development and Users Information, Vol. II-Programmers Manual,” AFFDL-TR-70-118, April 1971.
3. Wilkinson, K., Lerner, E., and Taylor, R. F., “Practical Design of Minimum Weight Aircraft Structures for Strength and Flutter Requirements,” AIAA Paper 74-986, Los Angeles, Calif., Aug. 1974.
4. Rudisill, C. S. and Bhatia, K. G., “Optimization of Complex Structures to Satisfy Flutter Requirements,” AIAA Journal, Vol. 9, Aug. 1971, pp. 1487-1491.
5. Wennagel, G. J., Loshigian, H. H., and Rosenbaum, J. D., “RAVES-Rapid Aerospace Vehicle Evaluation System,” Winter Annual Meeting of the American Society of Mechanical Engineers, Houston, Texas, Nov. 30-Dec. 5, 1975