Aerodynamic design of exo-skeletal engine fan blades

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 6, Issue , 2003, Pages 4226-4235

  Abumeri, Galib H ^a   Schmidt, James F ^a   Chamis, Christos C ^b  

^a QSS GROUP INC   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; CALCULATIONS; COMPUTER SIMULATION; EFFICIENCY; PERFORMANCE; ROTORS; SUBSONIC FLOW; TURBOMACHINE BLADES; TURBULENT FLOW;

ADIABATIC EFFICIENCY; AERODYNAMIC DESIGN; EXO-SKELETAL ENGINE; TURBULENT BOUNDARY LAYER SEPARATION;

AIRCRAFT ENGINES;

EID: 0042009687     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Halliwell, I.: "Exoskeletal Engine Concept: Feasibility Studies for Medium and Small Thrust Engines", NASA Contractor Report 2001-211322.
2. G. H. Abumeri and C. C. Chamis: "EST/BEST: a Computer Code for Assessing the Benefits of Advanced Aerospace Technologies", published in the journal of Advances in Engineering Software, 1997 Elsevier Science Limited, Printed in Great Britain., pp. 231-238.
3. A. J. Glassman and T. M. Lavelle: "Enhanced Capabilities and Modified Users Manual for Axial-Flow Compressor Conceptual Design code CSPAN", NASA TM 106833, 1995.
4. J. E. Crouse and W. T. Gorrell: "Computer Program for Aerodynamic and Blading Design of Multistage Axial-Flow Compressors", NASA TP 1946, published in 1981.
5. R. V. Chima: "RVCQ3D Rotor Viscous Code 3-D, User's Manual and Documentation", March 1999, NASA Glenn Research Center, Cleveland, Ohio
6. J. F. Schmidt: "Off-Design Computer Code for Calculating the Aerodynamic Performance of Axial-Flow Fans and Compressors User's Manual", NASA TM 198362, July 1995.