Modeling of the aircraft fatigue load environment

38th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2000, Pages

  Arrieta, Albert J ^a   Striz, Alfred G ^a  

^a UNIVERSITY OF OKLAHOMA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

NUMBER THEORY; PROBABILITY; RANDOM NUMBER GENERATION; REGRESSION ANALYSIS; SUPERSONIC AIRCRAFT;

CUMULATIVE FREQUENCIES; CUMULATIVE PROBABILITIES; EXPONENTIAL EQUATIONS; EXPONENTIAL POLYNOMIAL EQUATIONS; EXPONENTIAL POLYNOMIALS; PROBABILITY FUNCTIONS; PROBABILITY OF OCCURRENCE; RANDOM NUMBER GENERATORS;

POLYNOMIALS;

EID: 85087188354     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-973     Document Type: Conference Paper

References (9)

1. Kaplan, M. P., Reiman, J. A., and Landy, M. A., "Derivation of Flight-by-Flight Spectra for Fighter Aircraft, " Service Fatigue Loads, Monitoring, Simulation and Analysis, edited by P. R. Abelkis and J. M. Potter, ASTM 671, Philadelphia, Pennsylvania, November 1977, pg. 198.
2. Author unknown, Axum User's Guide, 3rd ed., Mathsoft Inc., Cambridge, Massachusetts, 1996.
3. Montgomery, D. C., Runger, G. C., and Hubele, N. F., Engineering Statistics, John Wiley & Sons, New York, 1998, pp. 322-324.
4. Arrieta, A., and Striz, A., "Normal Load Factor Data Regression Analyses, " AIAA/ASME Oklahoma Symposium, Oklahoma City, Feb. 1999.
5. Johnson, L. G., Theory and Technique of Variation Research, Elsevier Publishing Company, New York, 1964, pp. 1-6.
6. Rao, S. S., Reliability-Based Design, McGraw-Hill, New York, 1992, pp. 50-51.
7. Sandlin, N. H., Lauridia, R. R., and White, D. J., "Flight Spectra Development for Fighter Aircraft, " Service Fatigue Loads, Monitoring, Simulation and Analysis, edited by P. R. Abelkis and J. M. Potter, ASTM 671, Philadelphia, Pennsylvania, November 1977, pp. 144-157.
8. Denyer, A. G., "Flight-by-Flight Spectrum Development, " Service Fatigue Loads, Monitoring, Simulation and Analysis, edited by P. R. Abelkis and J. M. Potter, ASTM 671, Philadelphia, Pennsylvania, November 1977, pp. 158-175.
9. Author unknown, "Analysis Methods Document, " Repair Assessment Procedure And Integrated Design (RAPID), Version 2. 0, Appendix C, FAA, Atlantic City, New Jersey, July 1997, pp. C-10, C-11.