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Reynolds number effects on the performance of lateral control devices [microform] / Raymond E. Mineck ([NASA technical memorandum] ; NASA/TM-2000-210541)

Reynolds number effects on the performance of lateral control devices [microform] / Raymond E. Mineck ([NASA technical memorandum] ; NASA/TM-2000-210541)
Microform図書
2000<YCA-NAS 1.15:210541>
National Diet Library
  • Author HeadingMineck, Raymond E Langley Research Center

Assessment of dual-point drag reduction for an executive-jet modified airfoil section [microform] / Dennis O. Allison and Raymond E. Mineck (NASA technical paper ; 3579)

Assessment of dual-point drag reduction for an executive-jet modified airfoil section [microform] / Dennis O. Allison and Raymond E. Mineck (NASA technical paper ; 3579)
Microform図書
1996<YCA-NAS 1.60:3579>
National Diet Library
  • Author HeadingAllison, Dennis O Mineck, Raymond E Langley Research Center

Study of potential aerodynamic benefits from spanwise blowing at wingtip [microform] / Raymond E. Mineck (NASA technical paper ; 3515)

Study of potential aerodynamic benefits from spanwise blowing at wingtip [microform] / Raymond E. Mineck (NASA technical paper ; 3515)
Microform図書
1995<YCA-NAS 1.60:3515>
National Diet Library
  • Author HeadingMineck, Raymond E Langley Research Center

Application of two procedures for dual-point design of transonic airfoils [microform] / Raymond E. Mineck, Richard L. Campbell, and Dennis O. Allison (NASA technical paper ; 3466)

Application of two procedures for dual-point design of transonic airfoils [microform] / Raymond E. Mineck, Richard L. Campbell, and Dennis O. Allison (NASA technical paper ; 3466)
Microform図書
1994<YCA-NAS 1.60:3466>
National Diet Library
  • Author HeadingMineck, Raymond E Campbell, Richard L. (Richard...

Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line [microform] / Raymond E. Mineck, Paul M. H. W. Vijgen (NASA technical paper ; 3359)

Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line [microform] / Raymond E. Mineck, Paul M. H. W. Vijgen (NASA technical paper ; 3359)
Microform図書
1993<YCA-NAS 1.60:3359>
National Diet Library
  • Author HeadingMineck, Raymond E Vijgen, Paul M. H. W United S...

Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel microform / Raymond E. Mineck and Acquilla S. Hill (NASA technical paper ; 3049)

Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel microform / Raymond E. Mineck and Acquilla S. Hill (NASA technical paper ; 3049)
Microform図書
1990<YCA-NAS 1.60:3049>
National Diet Library
  • Author HeadingMineck, Raymond E Hill, Acquilla S United State...

Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel microform / Raymond E. Mineck (NASA technical memorandum ; 4114)

Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel microform / Raymond E. Mineck (NASA technical memorandum ; 4114)
Microform図書
1989<YCA-NAS 1.15:4114>
National Diet Library
  • Author HeadingMineck, Raymond E United States. National Aeron...

Experimental study on porous transonic airfoils with a view toward multipoint design AIAA-94-0500

Experimental study on porous transonic airfoils with a view toward multipoint design AIAA-94-0500
Paper規格・テクニカルリポート類
Hartwich, Peter M, Mineck, Raymond E<M-AIAA-94-0500>
National Diet Library

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