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 *

122 related articles for article (PubMed ID: 34852557)

  • 1. A new force-measuring balance for large-scale model in hypersonic wind tunnel.
    Wang Q; Li S; Gao H; Lv J; Zhang X; Liu W; Liu Z
    Rev Sci Instrum; 2021 Nov; 92(11):115005. PubMed ID: 34852557
    [TBL] [Abstract][Full Text] [Related]  

  • 2. A New Hypersonic Wind Tunnel Force Measurement System to Reduce Additional Bending Moment and Avoid Time-Varying Stiffness.
    Li S; Liu Z; Zhao F; Gao H
    Sensors (Basel); 2022 Mar; 22(7):. PubMed ID: 35408187
    [TBL] [Abstract][Full Text] [Related]  

  • 3. Hypersonic Aerodynamic Force Balance Using Micromachined All-Fiber Fabry⁻Pérot Interferometric Strain Gauges.
    Qiu H; Min F; Yang Y; Ran Z; Duan J
    Micromachines (Basel); 2019 May; 10(5):. PubMed ID: 31083493
    [TBL] [Abstract][Full Text] [Related]  

  • 4. Hypersonic force measurements using internal balance based on optical micromachined Fabry-Perot interferometry.
    Qiu H; Min F; Zhong S; Song X; Yang Y
    Rev Sci Instrum; 2018 Mar; 89(3):035004. PubMed ID: 29604776
    [TBL] [Abstract][Full Text] [Related]  

  • 5. A stereo photogrammetry system for model position and attitude measurement in hypersonic wind tunnel testing.
    Zhang M; Liang J; Chen L; Tang Z; Zong Y
    Rev Sci Instrum; 2021 Jul; 92(7):075107. PubMed ID: 34340425
    [TBL] [Abstract][Full Text] [Related]  

  • 6. Dynamic calibration and validation of an accelerometer force balance for hypersonic lifting models.
    Singh P; Trivedi S; Menezes V; Hosseini H
    ScientificWorldJournal; 2014; 2014():813759. PubMed ID: 24574921
    [TBL] [Abstract][Full Text] [Related]  

  • 7. Force measurement using strain-gauge balance in a shock tunnel with long test duration.
    Wang Y; Liu Y; Luo C; Jiang Z
    Rev Sci Instrum; 2016 May; 87(5):055108. PubMed ID: 27250471
    [TBL] [Abstract][Full Text] [Related]  

  • 8. Ultrasensitive all-fiber inline Fabry-Perot strain sensors for aerodynamic measurements in hypersonic flows.
    Xie Z; He X; Xiao Y; Yang T; Wang B; Ran Z; Rao Y; Min F; Qiu H; Yang Y; Chu W; Zeng D
    ISA Trans; 2020 Jul; 102():388-396. PubMed ID: 32113651
    [TBL] [Abstract][Full Text] [Related]  

  • 9. 3D Numerical Simulation and Structural Optimization for a MEMS Skin Friction Sensor in Hypersonic Flow.
    Guo H; Wang X; Liu T; Guo Z; Gao Y
    Micromachines (Basel); 2022 Sep; 13(9):. PubMed ID: 36144111
    [TBL] [Abstract][Full Text] [Related]  

  • 10. Intelligent Force-Measurement System Use in Shock Tunnel.
    Wang Y; Jiang Z
    Sensors (Basel); 2020 Oct; 20(21):. PubMed ID: 33142976
    [TBL] [Abstract][Full Text] [Related]  

  • 11. Development of an aerodynamic measurement system for hypersonic rarefied flows.
    Ozawa T; Fujita K; Suzuki T
    Rev Sci Instrum; 2015 Jan; 86(1):015105. PubMed ID: 25638120
    [TBL] [Abstract][Full Text] [Related]  

  • 12. Wind Tunnel Measurement Systems for Unsteady Aerodynamic Forces on Bluff Bodies: Review and New Perspective.
    Chen Z; Xu Y; Huang H; Tse KT
    Sensors (Basel); 2020 Aug; 20(16):. PubMed ID: 32824586
    [TBL] [Abstract][Full Text] [Related]  

  • 13. Measurements of Aerodynamic Interference of a Hybrid Aircraft with Multirotor Propulsion.
    Czyż Z; Wendeker M
    Sensors (Basel); 2020 Jun; 20(12):. PubMed ID: 32545745
    [TBL] [Abstract][Full Text] [Related]  

  • 14. Pressure-sensitive paint technique for surface pressure measurements in a low-density wind tunnel.
    Anyoji M; Numata D; Nagai H; Asai K
    J Vis (Tokyo); 2015; 18(2):297-309. PubMed ID: 25937803
    [TBL] [Abstract][Full Text] [Related]  

  • 15. Fabrication and Hypersonic Wind Tunnel Validation of a MEMS Skin Friction Sensor Based on Visual Alignment Technology.
    Wang X; Wang N; Xu X; Zhu T; Gao Y
    Sensors (Basel); 2019 Sep; 19(17):. PubMed ID: 31484311
    [TBL] [Abstract][Full Text] [Related]  

  • 16. MEMS Skin Friction Sensor with High Response Frequency and Large Measurement Range.
    Guo H; Wang X; Liu T; Guo Z; Gao Y
    Micromachines (Basel); 2022 Jan; 13(2):. PubMed ID: 35208358
    [TBL] [Abstract][Full Text] [Related]  

  • 17. Wind Tunnel Performance Tests of the Propellers with Different Pitch for the Electric Propulsion System.
    Czyż Z; Karpiński P; Skiba K; Wendeker M
    Sensors (Basel); 2021 Dec; 22(1):. PubMed ID: 35009545
    [TBL] [Abstract][Full Text] [Related]  

  • 18. Characterization of Freestream Disturbances in Conventional Hypersonic Wind Tunnels.
    Duan L; Choudhari MM; Chou A; Munoz F; Ali SRC; Radespiel R; Schilden T; Schröder W; Marineau EC; Casper KM; Chaudhry RS; Candler GV; Gray KA; Schneider SP
    J Spacecr Rockets; 2019 Mar; 56(2):357-368. PubMed ID: 33414565
    [TBL] [Abstract][Full Text] [Related]  

  • 19. Experimental Study of Aerodynamic Interference Effects for a Suspended Monorail Vehicle-Bridge System Using a Wireless Acquisition System.
    Zou Y; Liu Z; Shi K; Ou S; He X; Deng H; Zhou S
    Sensors (Basel); 2021 Aug; 21(17):. PubMed ID: 34502728
    [TBL] [Abstract][Full Text] [Related]  

  • 20. Wind Tunnel Measurements for Flutter of a Long-Afterbody Bridge Deck.
    Chen ZS; Zhang C; Wang X; Ma CM
    Sensors (Basel); 2017 Feb; 17(2):. PubMed ID: 28208773
    [TBL] [Abstract][Full Text] [Related]  

    [Next]    [New Search]
    of 7.