REFERENCES 



1. McCarthy, J.H. et al., "The Roles of Transition, Laminar Separation, and Turbulence 

 Stimulation in the Analysis of Axisymmetric Body Drag, " Eleventh Symposium on Naval 

 Hydrodynamics, London (1976). 



2. Granville, P.S., "Geometrical Characteristics of Noses and Tails for Parallel Middle 

 Bodies," NSRDC Report 3763 (Dec 1972). 



3. Granville, P.S., "Geometrical Characteristics of Flat-Faced Bodies of Revolution," 

 NSRDC Report 3710 (Nov 1971). 



4. Hess, J.L. and A.M.O. Smith, "Calculation of Potential Flow about Arbitrary 

 Bodies," Progress in Aeronautical Sciences, Vol. 8, Pergamon Press, Inc., New York (1966). 



5. Smith, A.M.O. and N. Gamberoni, "Transition Pressure Gradient and Stability 

 Theory," Douglas Aircraft Company Report ES-26388 (Aug 1956). 



6. Wazzan, A.R. et al., "Spatial and Temporal Stability Charts for the Flakner-Skan 

 Boundary-Layer Profiles," Douglas Aircraft Company Report DAC-67086 (Sep 1968). 



7. Curie, N. and S.W. Skan, "Approximate Methods for Predicting Separation 

 Properties of Laminar Boundary Layers," Aeronautical Quarterly, Vol. 8 ( 1957). 



8. Granville, P.S., "The Calculation of the Viscous Drag of Bodies of Revolution," 

 David Taylor Model Basin Report 849 (Jul 1953). 



9. Schlicting, H., "Boundary Layer Theory," McGraw-Hill, Inc., New York, Chapters 

 12, 16, and 17 (1955). 



10. Schubauer, G.B. and P.S. Klebanoff, "Contributions on the Mechanics of Boundary 

 Layer Transition," National Advisory Committee for Aeronautics TN 3849 (1955). 



1 1. Schoenherr, K.E., "Resistance of Flat Plates Moving through a Fluid," Transactions 

 of Society of Naval Architests and Marine Engineers, Vol. 40, (1932). 



12. von Kerczek, C. and N.C. Groves, "Disturbance Amplification in Boundary Layers," 

 paper in preparation. 



47 



