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Boundary layer transition in the leading edge region of a swept cylinder in high speed flow [microform] / Colin P. Coleman (NASA/TM ; 1998-112224)

Boundary layer transition in the leading edge region of a swept cylinder in high speed flow [microform] / Colin P. Coleman (NASA/TM ; 1998-112224)
Microform図書
1998<YCA-NAS 1.15:112224>
National Diet Library
  • Author HeadingColeman, Colin P Ames Research Center

A survey of theoretical and experimental coaxial rotor aerodynamic research [microform] / Colin P. Coleman (NASA technical paper ; 3675)

A survey of theoretical and experimental coaxial rotor aerodynamic research [microform] / Colin P. Coleman (NASA technical paper ; 3675)
Microform図書
1997<YCA-NAS 1.60:3675>
National Diet Library
  • Author HeadingColeman, Colin P Ames Research Center

Experimental and computational investigation of leading edge transition at Mach 1.6 AIAA-97-1776

Experimental and computational investigation of leading edge transition at Mach 1.6 AIAA-97-1776
Paper規格・テクニカルリポート類
Coleman, Colin P, Poll, D. I. A, Lin, Ray-Sing1997<M-AIAA-97-1776>
National Diet Library

Aerodynamic limitations of the UH-60A rotor [microform] / Colin P. Coleman, William G. Bousman (NASA technical memorandum ; 110396) (USAATCOM technical report ; 96-A-011)

Aerodynamic limitations of the UH-60A rotor [microform] / Colin P. Coleman, William G. Bousman (NASA technical memorandum ; 110396) (USAATCOM technical report ; 96-A-011)
Microform図書
1996<YCA-NAS 1.15:110396>
National Diet Library
  • Author HeadingColeman, Colin P Bousman, William G Ames Resea...

ATTACHMENT-LINE TRANSITION DUE TO ROUGHNESS ON A 76 DEGREE SWEPT CYLINDER AT MACH 1.6 (20000081770)

ATTACHMENT-LINE TRANSITION DUE TO ROUGHNESS ON A 76 DEGREE SWEPT CYLINDER AT MACH 1.6 (20000081770)
Paper図書
COLEMAN,COLIN P.(NASA GODDARD SPACE FLIGHT CENTER)1999.
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