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Angular Momentum on Longitudinal and Directional Stability in Steady Rolling Maneu-
vers:' NACA TN 4249, April 1958.
4Hacker, T., and Oprisiu, C., "A Discussion on the Roll Coupling Problem," Prog-ress in
Aerospace Sciences, Vol. 15, 1974, pp. 151-180,
sSchy, A. A., and Hannah, M. E., "Prediction of Jump Phenomena in Roll-Coupled Ma-
neuvers of Airplanes:' loumal of Aincraft, Vol. 14, No. 4, April 1977, pp. 375-382.
6Stemfield, L., "A Simplified Method for Approximating the Transient Motion in Angles
of Attack and Sideslip Dtmng Constant Rolling Maneuvcr:' NACA Rept. 1344, 1958.
/Blakelock, R. C.,Automatic ControL of Aircraft and Missiles, Wiley, New York, 1965.
8Knight, M., "Wind Tunnel Tests on the Autorotation and the Flat Spin:' NACA Rept.
273, 1927.
9Polhamus, E. C., iIEffect of Flow Incidence and Reynolds Number on Low Speed Aero-
dynamic Characteristics of Several Noncircular Cylinders with Application to Directional
Stability and Spinning:' NASA TR R-29, 1959.
IoAnderson, S. B., ' Historical Ovenniew of StaIVSpin Characteristics of General Aviation
Aircraft:' AIAA Paper 78-1551, Aug. 1978.
IIChambers, J. R., and Paul Stough, H., III., t*Summary of NASA Stall/Spin Research for
General Aviation Configurations:' AIAA Paper 86-2597, 1986.
r2DiCarl0, D. J., Stough, H. P., III., Glover, K. E., Brown, P. W., and Patton, J. M., Jr.,
"Development of Spin Resistance Criteria for General Aviation Airplanes," AIAA Paper
86-9812, 1986.
13Gates, S. B., and Bryant, L. W., isThe Spinning of Aeroplanes," ARC R and M No. 1001,
1926.
I4Pamadi, B. N., and Taylor, L. W., Jr., "A Semi-Empirical Method for Estimation of
Aerodynamic Characteristics of Steadily Spinning Light Airplanes:' NASA TM 4009, Dec.
1987.
15Pamadi, B. N., and Taylor, L. W., Jr., "Estimation of Aerodynamic Characteristics of
Steadily Spinning Light Airplanes:' Joumal of Aircrajt, Vol. 21, No. 12, 1984, pp. 943-
954.
16Adams, W. M., Jr., "Analytical Prediction of Airplane Equilibrium Spin Characteristics:'
NASA TN D-6926, Nov. 1972.
672 PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL
n Dickinson, B., Aircraft Stabiluy and Control for Prlots tmd Enginears, Sir Isaac Pitman
and Sons, London,1968.
18Beaurain, L., "General Study of Light Airplane Spin, Aft Geometry, Part I," NASA
TTF-17446, June 1977.
19Burk, S. M., Bowman, J. S., and White, W. L., "Spin-lhnnellnvestigation of the S pinning
Characteristics of Typical Single-Engine General Aviation Airplane Designs, I-Low Wing
Model A, Effect of Tail Configurations:' NASA TP 1009, 1977. .
20Airworthiness Standards, IINormal, Utility and Acrobatic Category Airplanes:' Federal
Aviation Regulations, Vol. III, Part 23, FAA, June 1974.
21 Neihouse, A.I., and Klinar, W. J., "Status of Spin Research for Recent Airplane Designs:'
NASA TR R-57, 1960 (Supersedes NACA RM L57F12).
22Bowman, J- S., "Summary of Spin Technology as Related to Light General Aviation
Airplanes:' NASA TFfD-7575, Dec. 1971.
23 Staff of Langley Research Center, "Exploratory Study of the Effects of Wing-Leading
Edge Modifications on the Stall/Spin Behavior of a Light General Aviation Airplane,"
NASA TP 2011, June 1982.
24DiCarlo, D. J., Glover, K. E., Stewart, E. C., and Stough, H. P., "Discontinuous Wing
Leading Edge to Enhance Spin Resistance:' Joumal of Aircraft, Vol. 22, No. 4, 1985, pp.
283-288.
2SStough, H. P., III., Jordan, F. L., Jr., DiCarlo, D. J., and Glover, K. E., "Leading-Edge
Design for Improved Spin Resistance of Wings Incorporating Conventional and Advanced
Aitfoils:' Society of Automotive Engineers, SAE Aerospace Technology Conference and
Exposition, Paper 830720, Long Beach, CA, Oct. 14-17, 1985.
26Pamadi, B. N., and Pordal, H. S., "Effect of Strakes on the Autorotational Characteristics
of Noncircular Cylinders:' Joumal of Aircraft, Vol. 24, No. 2, 1987, pp. 84-97.
2:'Pamadi, B. N., Jambunathan, V., and Rahman, A., "Control of Autorotational Character-
istiCs of Light-Airplane Fuselages:' Joumal of Aircrafr, Vol. 25, No. 8, 1988, pp. 695-701.
Problems
7.1 If the aircraft in Example 7.1 is flying at 175 m/s at an altitude of 8000 m,
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