Davis and Oates 



3. Perkins and Hage: Airplane Performance Stability and Control. 



4. Glbbs and Cox: Hydrofoil Handbook. 



5. Glauert: Aerofoil and Airscrew Theory, 



6. Silverstein and Katzoff: Design Charts for Predicting Downwash Angles 

 and Wake Characteristics Behind Plain and Flapped Wings. NACA TR 648. 

 1940. 



7. Ribner: Notes on the Propeller and Slipstream in Relation to Stability. 

 NACA ARR L41 12a. (WR L-25) 1944. 



8. Michael, W. H., Jr.: Analysis of the Effects of Wing Interference on the 

 Tail Contributions to the Rolling Derivatives. NACA TN 2332 (also TR 

 1086) 1951. 



9. Campbell and McKinney: Summary of the Methods for Calculating Dynamic 

 Lateral Stability and Response and for Estimating Lateral Stability Deriva- 

 tives. NACA TR 968. 1950. 



10. Toll and Quijo: Approximate Relations and Charts for Low Speed Stability 

 Derivatives of Swept Wings. NACA TN 1581. 1948. 



11. Imlay: Theoretical Motions of Hydrofoil Systems. 1948. NACA TR 918. 



12. De Young and Harper: Theoretical Symmetric Span Loading at Subsonic 

 Speeds for Wings Having Arbitrary Plan Form. NACA TR 921. 



13. De Young: Theoretical Antisymmetric Span Loading at Subsonic Speeds for 

 Wings Having Arbitrary Plan Form. NACA TR 1056. 1951. 



14. Jones, R. T.: The Unsteady Lift of a Wing of Finite Aspect Ratio. NACA 

 R681. 



15. Tobak, M.: On the Use of the Indicial Function Concept in the Analysis of 

 Unsteady Motion of Wings and Wing- Tail Combinations. NACA R 1188. 

 1954. 



16. Drischler, J. A.: Approximate Indicial Lift Functions for Several Wings of 

 Finite Span in Incompressible Flow as obtained from Oscillatory Lift Co- 

 efficients. NACA TN 3639. 1936. 



17. Wadlin, K. L., Shufford, C. L., McGehee, J. R.: A Theoretical and Experi- 

 mental Investigation of the Lift and Drag Characteristics of a Hydrofoil at 

 Sub- Critical and Super -Critical Speed. NACA TR 1232. 1955. 



18. Brown, P. W.: Force Characteristics of Surface Piercing Fully Ventilated 

 Dihedral Hydrofoils. S.I.T. Report No. 698. Oct. 1958. 



652 



