Structural stability of a stiffened aluminum fuselage panel subjected to combined mechanical and internal pressure loads

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Volumn , Issue , 2003, Pages

  Rouse, Marshall ^a   Young, Richard D ^a   Gehrki, Ralph E ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b LOCKHEED MARTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM PANEL; ANALYTICAL STUDIES; BUCKLING LOADS; FUSELAGE PANELS; LOADING CONDITION; NON-LINEAR FINITE-ELEMENT ANALYSIS; PRESSURE LOADING; STRUCTURAL STABILITIES;

ALUMINUM; FINITE ELEMENT METHOD; FUSELAGES; LOADS (FORCES); STABILITY; STRESS CONCENTRATION; STRUCTURAL DYNAMICS;

BUCKLING;

EID: 84896693555     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Mahler, M., Ley, R., Shah, C., Lin, W., and Rouse, M., "Propagation and Control of Crack-Like Damage in Curved Composite Panels Under Combined Loads, " 41st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference & Exhibit, AIAA-2000-1533, April 3-6, 2000.
2. Ambur, D. A., Rouse, M., Starnes, J. H., and Shuart, M. J., "Facilities for Combined Loads Testing of Aircraft Structures to Satisfy Structural Technology Development Requirements, " presented at the 5th Annual Advanced Composites Technology Conference, Seattle, WA, August 22-36, 1994.
3. Ambur, D. R., Cerro, J. A., and Dickson, J. D., "DBox Fixture for Testing Stiffened Panels in Compression and Pressure, " Journal of Aircraft, Vol. 32, No. 6, Nov.-Dec. 1995, pp. 1382-1389.
4. Anon., PATRAN Plus User Manual-Release 3. 0, PDA Engineering, Publication Number 2191023, September 1989.
5. Rankin, C. C., Brogan, F. A., Loden, W. A., and Cabiness, H. K., "STAGS Users Manual, " Version 3. 0, Lockheed Martin Missiles & Space Co., Inc., Advanced Technology Center, Report LMSC P032594, 2001.