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　 冩梢胎猟僉鹿
　廨旋窟苧猟僉鹿　
　　
 
　
　		  
 

VOLUME I

AERODYNAMICS , FLUID MECHANICS
AND
MASS AND HEAT TBANSFER

　　l. Note on the Characteristics of Low Drag Airfoil,Chinese　Institute of Engineers Journal, Vol. 4, No. l, pp. 46-48,May, 1946 .
　　2. A Theoretical Investigation of the Temperature Field in the　Laminar Boundary Layer on a Porous Flat Plate with Fluid　Injection, Project SQUID ,Technical Report No. 4 , September 1947 .
　　3. Heat Transfer in Laminar Compressible Boundary Layer on a　Porous Flat Plate with Fluid Injection,J.A.S. Vol. 6, No.12,pp 741-748, December 1949.
　　4. Laminar Pipe Flow with Injection and Suction Through a Porous　Wall,Transactions A.S.M.E. , Vol. 78, No. 4, pp 719-724,May 1956.
　　5. Heat Transfer of a Laminar Pipe Flow with Coolant Injection,Jet Propuision, Vol. 28, No. 3, pp 178-181, March 1958
　　6. Transpiration Cooling in the Turbulent Flow Through a Porous　Wall Pipe, Proceedings of the 9th International Congress　of Applied Mechanics. Vol. II, pp. 331-340, September 1956.
　　7. Experimental Investigation of Transpiration Cooling in the　Torbulent Flow with Coolant Injection, Proceedings of 1958　Heat Transfer and Fluid Mechanics Institute, June 1958 .
　　8. Turbuient Flow in ChanneLs with Porous Wall, Journal oF　Mathematics and Physics, Vol. 38, No. 3, pp.166-171, Oct. 1959.
　　9. Turbulent Flow in a Circular Pipe with Porous Wall, The　Physics of Fluids, Vol. 4, No. 3, pp. 368-372, March 1961.
　　1O. Laminar Nonisothermal Pipe Flow with coolant Injection at　Wall, International Development in Heat Transfer, Part IV,PP. 717-724, August 1961.
　　11. Heat Transfer in Turbulent Pipe Flow with Coolant Injection,Developments in Mechanics. Vol. l, pp. 526-531,Plenum　Press , 1961 .
　　12. Laminar Nonisothermal Flow in Pipes with WalL Coolant　Injectionl Journal oF Polytechnic Institute of Jassy, Vol. 8 ,No.12, pp. 351-362 , 1962



AERODYNAMICS , FLIUD MECHANICS
AND
MASS AND HEAT TRANSFER

　　13. Turbulent Flow in a Porous-Wall Pipe, The Physics of Fluids,Vol. 5, No. IO. p.1312, October 1962.
　　14. Laminar Pipe Flow with Mass Transfer Cooling, Journal of　Heat Transfer, ASME, Vol. 87, Series C. No. 2, pp.252-85,May 1965.
　　15. Laminar Flow in the Entrance Region of a Porous-Wall　Channel, Applied Scientific Research, Section A, Vol. 14.pp. 233-48, 1965 .
　　16. Heat and Mass Transfer in Laminar Pipe Flow with Thermodyamic　Coupling Effects, Proceedings of First Canadian Congree ofApplied Mechanics, Vol. 2b, pp. 344-45, May 1967.
　　17. Jet Circulation Control Airfoil for VTOL Rotors, Journal　of Aircraft,AIAA, Vol. 7, No. 5. pp417-23, September 1970.
　　18. Experimental Investigation of Wing-Tip Vortices Elimination,Proceedings of Third Canadian Congress of Applied Mechanics,pp. 613-14, May 1971.
　　19. Vortex Pollution - Wing-Tip Vortices : The Hazard and the　Remedy, Journal of Aeronautical Society of India, Vol. 23,No. 2, pp. 67-70, May 1971.
　　20. Effect of Thermodynamic Coupling on Mass Transfer Cooling.Journal of the Aeronautical Society of India, Vol. 23,No. 4, pp. 174-82, November 1971.
　　21. Experimental Investigation of Wing-Tip Vortex Abatement.Proceedings of the IXth Congress of the International Council of Aeronautical Sciences ,Vol. l , pp. 303-Il ,
August 1974.

STRUCTURES , VIBRATION AND FLUTTER

　　1. Contributions to the Rotor Blade Desiqn, Chinese Institute　of Engineers Journal, vol. 3, No. l, pp.49-64, May 1945.
　　2. Thin Cylindrical Shell Subjected to Concentrated Loads.Quarterly of Applied Mathematics , Vol . IV, No. l ,pp. 13-26 .April 1946.
　　3. Bending of Rotor Blade in the Plane of Rotation, Journal of　the Aeronautival Sciences. Vol. 14, No. 51 pp. 285-93,May 1947.
　　4. Seaplane Flutter Analysis. Chinese Institute of Engineers　Journalr Vol. 5, No. 2, pp. 121-33, November 1947.
　　5. On Radial Deflections of a Cylinder Subjected to Equal and　Opposite Concentrated Radial Loads , Journal of Applied　Mechanics, ASME, pp. 278-82, July 1957.
　　6. On Radial Deflection of a Cylinder of Finite-Length with　Various End Conditions, Journal of Aeronautical Sciences ,Vol. 25, No. 4, Pp. 230-34. April 1958.
　　7. Thin Cylindrical Shells Subjected to Concentrated Surface　Torques, AIAA Journal, Vol. 3, No.l, pp. 178-80, Jan. 1965.


HELICOPTER ROTOR : AERODYNAMICS . STRUCTURES
AND
DYNAMICS OF STABILITY


　　l. Stability of Rotor Blade Flapping Motion When the Hinges　are Titled: ceneralization of the "Rectangular Ripple"　Method of Solution, Journal of the Aeronautical Sciences ,Vol. 14, No. 10, pp. 583-93, Ocotber 1947.
　　2. On the Stability of the Transient Motion of Helicopter　Bladss in Flapping and Lagging, Reissner Anniversary Volume ,pp.163-81, January 1949.
　　3. Preliminary Investigation of Karman-Yuan Helicopter Rotor　System, Proceedings of the 11th Annual Forum, American　Helicopter Society, April 1955.
　　4. Vibration of the Helicopter Rotor Fuselage System Induced　by the Main Rotor Blade in Flight, Journal of Applied　Mechanics, Vol. 22, No. 3, pp. 355-60, September 1955.
　　5. The Yuan Rotor System - A New Concept of VTOL.
　　6. Comparison of Power Required Between Conventional Rotor　and the Yuan Rotor Syatems.
　　7. Note on the Section Drag and Critical Mach Number of the　Jet Circulation Control Airfoil.

 
　PREFACE　　VOLUME I　　VOLUME II