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Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system [microform] / J.R. DeBonis and C.J. Trefny ([NASA technical memorandum] ; NASA/TM-2001-210567)

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system [microform] / J.R. DeBonis and C.J. Trefny ([NASA technical memorandum] ; NASA/TM-2001-210567)
Microform図書
2001<YCA-NAS 1.15:210567>
National Diet Library
  • Author HeadingDeBonis, J. R Trefny, C. J NASA Glenn Research Center

Analysis of a new rocket-based combined-cycle engine concept at low speed AIAA-99-2393

Analysis of a new rocket-based combined-cycle engine concept at low speed AIAA-99-2393
Paper規格・テクニカルリポート類
Yungster, S, Trefny, C. J1999<M-AIAA-99-2393>
National Diet Library

Analysis of a new rocket-based combined-cycle engine concept at low speed [microform] / S. Yungster, C.J. Trefny (NASA/TM ; 1999-209393)

Analysis of a new rocket-based combined-cycle engine concept at low speed [microform] / S. Yungster, C.J. Trefny (NASA/TM ; 1999-209393)
Microform図書
1999<YCA-NAS 1.15:209393>
National Diet Library
  • Author HeadingYungster, S Trefny, C. J NASA Glenn Research Center

Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics [microform] / J.R. DeBonis, C.J. Trefny, and C.J. Steffen, Jr (NASA/TM ; 1999-209279)

Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics [microform] / J.R. DeBonis, C.J. Trefny, and C.J. Steffen, Jr (NASA/TM ; 1999-209279)
Microform図書
1999<YCA-NAS 1.15:209279>
National Diet Library
  • Author HeadingDeBonis, J. R Trefny, C. J Steffen, C. J NASA Glenn Rese...

Semiempirical Method of Determining Flow Coefficients for Pitot Rake Mass Flow Rate Measurements NASA-TM-87144 N86-14219 NAS-11587144 E-2772

Semiempirical Method of Determining Flow Coefficients for Pitot Rake Mass Flow Rate Measurements NASA-TM-87144 N86-14219 NAS-11587144 E-2772
Microform規格・テクニカルリポート類
Trefny, C. J<LS-N86/14219>
National Diet Library

Experiments and Analysis Concerning the Use of External Burning to Reduce Aerospace Vehicle Transonic Drag. Ph.D. Thesis NASA-TM-105397 N92-17546 NAS-115105397 E-6789

Experiments and Analysis Concerning the Use of External Burning to Reduce Aerospace Vehicle Transonic Drag. Ph.D. Thesis NASA-TM-105397 N92-17546 NAS-115105397 E-6789
Microform規格・テクニカルリポート類
Trefny, C. J<LS-N92/17546>
National Diet Library

Use of External Burning to Reduce Aerospace Vehicle Transonic Drag NASA-TM-103107 N90-21762 NAS-115103107

Use of External Burning to Reduce Aerospace Vehicle Transonic Drag NASA-TM-103107 N90-21762 NAS-115103107
Microform規格・テクニカルリポート類
Trefny, C. J<LS-N90/21762>
National Diet Library

Low-Speed Performance of an Axisymmetric, Mixed-Compression, Supersonic Inlet with Auxiliary Inlets NASA-TP-2557 N86-24694 NAS-1602557 E-2771

Low-Speed Performance of an Axisymmetric, Mixed-Compression, Supersonic Inlet with Auxiliary Inlets NASA-TP-2557 N86-24694 NAS-1602557 E-2771
Microform規格・テクニカルリポート類
Trefny, C. J, Wasserbauer, J. W<LS-N86/24694>
National Diet Library

Low Speed Performance of a Supersonic Axisymmetric Mixed Compression Inlet with Auxiliary Inlets NASA-TM-83435 N83-27992 NAS-11583435 E-1730

Low Speed Performance of a Supersonic Axisymmetric Mixed Compression Inlet with Auxiliary Inlets NASA-TM-83435 N83-27992 NAS-11583435 E-1730
Microform規格・テクニカルリポート類
Wasserbauer, J. F, Cubbison, R. W, Trefny, C. J<LS-N83/27992>
National Diet Library

Low-Speed Aerodynamic Test of an Axisymmetric Supersonic Inlet with Variable Cowl Slot NASA-TM-87039 N85-26710 NAS-11587039 E-2595

Low-Speed Aerodynamic Test of an Axisymmetric Supersonic Inlet with Variable Cowl Slot NASA-TM-87039 N85-26710 NAS-11587039 E-2595
Microform規格・テクニカルリポート類
Powell, A. G, Welge, H. R, Trefny, C. J<LS-N85/26710>
National Diet Library

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