These tools will no longer be maintained as of December 31, 2024. Archived website can be found here. PubMed4Hh GitHub repository can be found here. Contact NLM Customer Service if you have questions.


BIOMARKERS

Molecular Biopsy of Human Tumors

- a resource for Precision Medicine *

142 related articles for article (PubMed ID: 28669688)

  • 1. Effect of an upstream bulge configuration on film cooling with and without mist injection.
    Wang J; Li Q; Sundén B; Ma T; Cui P
    J Environ Manage; 2017 Dec; 203(Pt 3):1072-1079. PubMed ID: 28669688
    [TBL] [Abstract][Full Text] [Related]  

  • 2. Numerical investigation of mist/air impingement cooling on ribbed blade leading-edge surface.
    Bian Q; Wang J; Chen YT; Wang Q; Zeng M
    J Environ Manage; 2017 Dec; 203(Pt 3):1062-1071. PubMed ID: 28545948
    [TBL] [Abstract][Full Text] [Related]  

  • 3. Experimental and Numerical Investigations of Effects of Flow Control Devices Upon Flat-Plate Film Cooling Performance.
    Kawabata H; Funazaki KI; Nakata R; Takahashi D
    J Turbomach; 2014 Jun; 136(6):0610211-6102111. PubMed ID: 25278646
    [TBL] [Abstract][Full Text] [Related]  

  • 4. Finite element analysis of flowfield in the single hole film cooling technique.
    Bazdidi-Tehrani F; Mahmoodi AA
    Ann N Y Acad Sci; 2001 May; 934():393-400. PubMed ID: 11460653
    [TBL] [Abstract][Full Text] [Related]  

  • 5. Contribution of heat transfer to turbine blades and vanes for high temperature industrial gas turbines. Part 1: Film cooling.
    Takeishi K; Aoki S
    Ann N Y Acad Sci; 2001 May; 934():305-12. PubMed ID: 11460641
    [TBL] [Abstract][Full Text] [Related]  

  • 6. Film cooling performance on curved walls with compound angle hole configuration.
    Chen PH; Hung MS; Ding PP
    Ann N Y Acad Sci; 2001 May; 934():353-60. PubMed ID: 11460647
    [TBL] [Abstract][Full Text] [Related]  

  • 7. Enhancement of Film Cooling Effectiveness in a Supersonic Nozzle.
    Somasekharan N; Srikrishnan AR; Kumar HS; Ganesh KP; Mohammad A; Velamati RK
    Entropy (Basel); 2023 Mar; 25(3):. PubMed ID: 36981371
    [TBL] [Abstract][Full Text] [Related]  

  • 8. Effect of turbulence intensity on cross-injection film cooling at a stepped or smooth endwall of a gas turbine vane passage.
    Wu PS; Tsai ST; Jhuo YH
    ScientificWorldJournal; 2014; 2014():256136. PubMed ID: 24592153
    [TBL] [Abstract][Full Text] [Related]  

  • 9. Interaction Mechanism and Loss Analysis of Mixing between Film Cooling Jet and Passage Vortex.
    Chen Z; Hu K; Mao Y; Su X; Yuan X
    Entropy (Basel); 2021 Dec; 24(1):. PubMed ID: 35052041
    [TBL] [Abstract][Full Text] [Related]  

  • 10. Experimental investigation of film cooling flow induced by shaped holes on a turbine blade.
    Barthet S; Bario F
    Ann N Y Acad Sci; 2001 May; 934():313-20. PubMed ID: 11460642
    [TBL] [Abstract][Full Text] [Related]  

  • 11. Film cooling from rows of holes--effect of cooling hole shape and row arrangement on adiabatic effectiveness.
    Dittmar J; Jung IS; Schulz A; Wittig S; Lee JS
    Ann N Y Acad Sci; 2001 May; 934():321-8. PubMed ID: 11460643
    [TBL] [Abstract][Full Text] [Related]  

  • 12. Particle Deposition in the Vicinity of Multiple Film Cooling Holes.
    Peng Y; Xu G; Luo X; He J; Liu D
    Micromachines (Basel); 2022 Mar; 13(4):. PubMed ID: 35457826
    [TBL] [Abstract][Full Text] [Related]  

  • 13. Investigations on the effect of different influencing factors on film cooling effectiveness under the injection of synthetic coolant.
    Chang J; Duan X; Du Y; Guo B; Pan Y
    Sci Rep; 2021 Feb; 11(1):3408. PubMed ID: 33564082
    [TBL] [Abstract][Full Text] [Related]  

  • 14. Optimization of the Double-Expansion Film-Cooling Hole Using CFD.
    Zhang Z; Hu T; Su X; Yuan X
    Entropy (Basel); 2023 Feb; 25(3):. PubMed ID: 36981300
    [TBL] [Abstract][Full Text] [Related]  

  • 15. The variation of heat transfer coefficient, adiabatic effectiveness and aerodynamic loss with film cooling hole shape.
    Sargison JE; Guo SM; Oldfield ML; Rawlinson AJ
    Ann N Y Acad Sci; 2001 May; 934():361-8. PubMed ID: 11460648
    [TBL] [Abstract][Full Text] [Related]  

  • 16. INVESTIGATION OF SPIRAL AND SWEEPING HOLES.
    Thurman D; Culley D; Poinsatte P; Raghu S; Ameri A; Shyam V
    J Turbomach; 2016 Sep; 138(9):. PubMed ID: 31534303
    [TBL] [Abstract][Full Text] [Related]  

  • 17. Evaluation of 2 Heat-Mitigation Methods in Army Trainees.
    Sefton JM; McAdam JS; Pascoe DD; Lohse KR; Banda RL; Henault CB; Cherrington AR; Adams NE
    J Athl Train; 2016 Nov; 51(11):936-945. PubMed ID: 27710091
    [TBL] [Abstract][Full Text] [Related]  

  • 18. Variable refrigerant flow cooling assessment in humid environment using different refrigerants.
    Saab R; Al Quabeh H; Hassan Ali MI
    J Environ Manage; 2018 Oct; 224():243-251. PubMed ID: 30055457
    [TBL] [Abstract][Full Text] [Related]  

  • 19. Conjugate heat transfer study of various cooling structures and sensitivity analysis of overall cooling effectiveness.
    Liu R; Li H; You R; Huang Y; Tao Z
    Sci Rep; 2022 Nov; 12(1):19271. PubMed ID: 36357541
    [TBL] [Abstract][Full Text] [Related]  

  • 20. Uncertainty Quantification of Film Cooling Performance of an Industrial Gas Turbine Vane.
    Gamannossi A; Amerini A; Mazzei L; Bacci T; Poggiali M; Andreini A
    Entropy (Basel); 2019 Dec; 22(1):. PubMed ID: 33285791
    [TBL] [Abstract][Full Text] [Related]  

    [Next]    [New Search]
    of 8.