Fuel slosh in skewed tanks

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 5, 1996, Pages 1172-1177

  Abzug, Malcolm J ^a,b  

^a ACA Systems   (United States)

^b AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; EQUATIONS OF MOTION; FLIGHT DYNAMICS; FUEL TANKS; GRAVITATION; LINEARIZATION; MATHEMATICAL MODELS;

BOEING AIRPLANE; DUTCH ROLL MODE; FUEL SLOSH; GRAVITY FIXITY; PITCH ATTITUDE RANGE; SKEWED TANKS; WING DIHEDRAL;

FUEL SLOSHING;

EID: 0030241257     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21760     Document Type: Article

References (8)

1. Abzug, M. J., "Effects of Fuel Slosh on Stability and Control," Douglas Aircraft Co., Rept. No. ES 29551, Long Beach, CA, July 1959.
2. Graham, E. W., "The Forces Produced by Fuel Oscillation in a Rectangular Tank," Douglas Aircraft Co., Rept. No. SM 13748, Long Beach, CA, April 1950.
3. Lamb, H., Hydrodynamics, 6th ed., Dover, New York, 1945, pp. 282, 284.
4. Schy, A. A., "A Theoretical Analysis of the Effects of Fuel Motion on Airplane Dynamics," NACA Rept. 1080, 1952.
5. Luskin, H., and Lapin, E.,"An Analytical Approach to the Fuel Sloshing and Buffeting Problems of Aircraft," Journal of the Aeronautical Sciences, Vol. 8, No. 4, 1952, pp. 217-228.
6. McRuer, D., Ashkenas, I., and Graham, D., Aircraft Dynamics and Automatic Control, Princeton Univ. Press, Princeton, NJ, 1973, p. 295.
7. Heffley, R. K., and Jewell, W. F., "Aircraft Handling Qualities Data," NASA CR-2144, Dec. 1972.
8. McRuer, D. T., and Johnston, D. E., "Flight Control Systems Properties and Problems, Vol. I," NASA CR-2500, Feb. 1975.