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1. Sinnette, John T. Analysis of effect of basic design variables on subsonic axial-flow-compressor performance Washington: U. S. Govt. Print. Off., 1948 [i. e]; [1949]

 BIBFRAME Instances
 Instance 8367607
2. Torda, T. Paul, 1911- Analysis of viscous laminar incompressible flow through axial flow turbomachines with infintesimal blade spacing [Urbana]: [University of Illinois]; [1952]

 BIBFRAME Instances
 Instance 8387209
3. Wu, Min-hua (Li) Analysis of plane-plastic-stress problems with axial symmetry in strain-hardening range Washington: U. S. Govt. Print Off; 1951

 BIBFRAME Instances
 Instance 6037920
4. Sanders, John C. Equilibrium operating performance of axial-flow turbojet engines by means of idealized analysis Washington: U. S. Govt. Print. Off; 1950

 BIBFRAME Instances
 Instance 10246355
5. Tennyson, Roderick C. (Roderick Clarence), 1937- Analysis of the buckling process of circular cylindrical shells under axial compression [Toronto]: [Institute for Aerospace Studies, University of Toronto]; 1968

 BIBFRAME Instances
 Instance 1711116
6. Aungier, Ronald H. Axial-flow compressors New York: ASME Press; 2003

 BIBFRAME Instances
 Instance 12962864
7. Zou, Zhengping Axial Turbine Aerodynamics for Aero-engines Singapore: Springer Singapore, Imprint: Springer; 2018

 BIBFRAME Instances
 Instance 21937702
8. Torda, T. Paul, 1911- Analysis of viscous laminar incompressible flow through axial flow turbomachines with infintesimal blade spacing

 BIBFRAME Works
 Work
Text
Monograph		 8387209
9. Wu, Min-hua (Li) Analysis of plane-plastic-stress problems with axial symmetry in strain-hardening range

 BIBFRAME Works
 Work
Text
Monograph		 6037920
10. Tennyson, Roderick C. (Roderick Clarence), 1937- Analysis of the buckling process of circular cylindrical shells under axial compression

 BIBFRAME Works
 Work
Text
Monograph		 1711116
11. Sinnette, John T. Analysis of effect of basic design variables on subsonic axial-flow-compressor performance

 BIBFRAME Works
 Work
Text
Monograph		 8367607
12. Sanders, John C. Equilibrium operating performance of axial-flow turbojet engines by means of idealized analysis

 BIBFRAME Works
 Work
Text
Monograph		 10246355
13. Aungier, Ronald H. Turbine aerodynamics New York: ASME Press; c2006

 BIBFRAME Instances
 Instance 14102053


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