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Dive into the research topics where Brian H. Houston is active.

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Featured researches published by Brian H. Houston.


Applied Physics Letters | 2002

Nanomechanical resonant structures in nanocrystalline diamond

Lidija Sekaric; J. M. Parpia; Harold G. Craighead; T. Feygelson; Brian H. Houston; James E. Butler

We report the fabrication and the operation of nanomechanical resonant structures in nanocrystalline diamond. For this purpose, continuous diamond films as thin as 80 nm were grown using microwave plasma enhanced chemical vapor deposition. The lateral dimensions of the fabricated structures were as small as 50 nm and the measured mechanical resonant frequencies were up to 640 MHz. The mechanical quality factors were in the range of 2500–3000 at room temperature. The elastic properties of these films obtained via the resonant measurements indicate a Young’s modulus close to that of single-crystal diamond.


Applied Physics Letters | 2002

Thermoelastic loss in microscale oscillators

Brian H. Houston; Douglas M. Photiadis; Martin H. Marcus; J. A. Bucaro; Xiao Liu; Joseph F. Vignola

A simple model of thermoelastic dissipation is proposed for general, free standing microelectromechanical (MEMS) and nanoelectromechanical (NEMS) oscillators. The theory defines a flexural modal participation factor, the fraction of potential energy stored in flexure, and approximates the internal friction by assuming the energy loss to occur solely via classical thermoelastic dissipation of this component of the motion. The theory is compared to the measured internal friction of a high Q mode of a single-crystal silicon double paddle oscillator. The loss at high temperature (above 150 K) is found to be in good agreement with the theoretical prediction. The importance of this dissipation mechanism as a function of scale is briefly discussed. We find that the relative importance of this mechanism scales with the size of the structure, and that for nanoscale structures it is less important than intrinsic phonon–phonon scattering.


ACS Nano | 2012

Surface Doping and Bandgap Tunability in Hydrogenated Graphene

Jeffrey W. Baldwin; Bernard R. Matis; James S. Burgess; Felipe Bulat-Jara; Adam L. Friedman; Brian H. Houston

We report the first observation of the n-type nature of hydrogenated graphene on SiO(2) and demonstrate the conversion of the majority carrier type from electrons to holes using surface doping. Density functional calculations indicate that the carrier type reversal is directly related to the magnitude of the hydrogenated graphenes work function relative to the substrate, which decreases when adsorbates such as water are present. Additionally, we show by temperature-dependent electronic transport measurements that hydrogenating graphene induces a band gap and that in the moderate temperature regime [220-375 K], the band gap has a maximum value at the charge neutrality point, is tunable with an electric field effect, and is higher for higher hydrogen coverage. The ability to control the majority charge carrier in hydrogenated graphene, in addition to opening a band gap, suggests potential for chemically modified graphene p-n junctions.


Applied Physics Letters | 2006

Effect of viscous loss on mechanical resonators designed for mass detection

Joseph F. Vignola; John A. Judge; Jacek Jarzynski; Maxim Zalalutdinov; Brian H. Houston; Jeffrey W. Baldwin

Simple models are presented for estimating viscous damping of fluid (gas or liquid) loaded mechanical resonators. The models apply to beams in flexural modes of vibration, and to thin beams and plates in longitudinal modes of vibration. Predictions of the associated quality factor are compared with measured values for several macroscale and microscale resonators. The scaling of viscous loss with oscillator size is discussed. The minimum detectable mass is estimated for several oscillator designs and it is shown that, for comparably sized devices, longitudinal resonators have the lowest threshold of detection. This minimum detectable mass is proportional to scale to the power 1.75 for all resonator architectures limited by viscous damping, and it is shown that the viscous loss is 220 times larger in water than in air.


Journal of the Acoustical Society of America | 2003

Fast Fourier transform and singular value decomposition formulations for patch nearfield acoustical holography

Earl G. Williams; Brian H. Houston; Peter C. Herdic

Nearfield acoustical holography (NAH) requires the measurement of the pressure field over a complete surface in order to recover the normal velocity on a nearby concentric surface, the latter generally coincident with a vibrator. Patch NAH provides a major simplification by eliminating the need for complete surface pressure scans-only a small area needs to be scanned to determine the normal velocity on the corresponding (small area) concentric patch on the vibrator. The theory of patch NAH is based on (1) an analytic continuation of the patch pressure which provides a spatially tapered aperture extension of the field and (2) a decomposition of the transfer function (pressure to velocity and/or pressure to pressure) between the two surfaces using the singular value decomposition (SVD) for general shapes and the fast Fourier transform (FFT) for planar surfaces. Inversion of the transfer function is stabilized using Tikhonov regularization and the Morozov discrepancy principle. Experimental results show that root mean square errors of the normal velocity reconstruction for a point-driven vibrator over 200-2700 Hz average less than 20% for two small, concentric patch surfaces 0.4 cm apart. Reconstruction of the active normal acoustic intensity was also successful, with less than 30% error over the frequency band.


Journal of the Acoustical Society of America | 2000

Interior near-field acoustical holography in flight

Earl G. Williams; Brian H. Houston; Peter C. Herdic; S. T. Raveendra; Bryce K. Gardner

In this paper boundary element methods (BEM) are mated with near-field acoustical holography (NAH) in order to determine the normal velocity over a large area of a fuselage of a turboprop airplane from a measurement of the pressure (hologram) on a concentric surface in the interior of the aircraft. This work represents the first time NAH has been applied in situ, in-flight. The normal fuselage velocity was successfully reconstructed at the blade passage frequency (BPF) of the propeller and its first two harmonics. This reconstructed velocity reveals structure-borne and airborne sound-transmission paths from the engine to the interior space.


Nano Letters | 2012

Shear Modulus of Monolayer Graphene Prepared by Chemical Vapor Deposition

Xiao Liu; Thomas Metcalf; Jeremy T. Robinson; Brian H. Houston; Fabrizio Scarpa

We report shear modulus (G) and internal friction (Q(-1)) measurements of large-area monolayer graphene films grown by chemical vapor deposition on copper foil and transferred onto high-Q silicon mechanical oscillators. The shear modulus, extracted from a resonance frequency shift at 0.4 K where the apparatus is most sensitive, averages 280 GPa. This is five times larger than those of the multilayered graphene-based films measured previously. The internal friction is unmeasurable within the sensitivity of our experiment and thus bounded above by Q(-1) ≤ 3 × 10(-5), which is orders-of-magnitude smaller than that of multilayered graphene-based films. Neither annealing nor interface modification has a measurable effect on G or Q(-1). Our results on G are consistent with recent theoretical evaluations and simulations carried out in this work, showing that the shear restoring force transitions from interlayer to intralayer interactions as the film thickness approaches one monolayer.


Journal of Applied Physics | 2007

Attachment loss of micromechanical and nanomechanical resonators in the limits of thick and thin support structures

John A. Judge; Douglas M. Photiadis; Joseph F. Vignola; Brian H. Houston; Jacek Jarzynski

Analytical expressions are provided for the energy loss from vibrating mechanical resonators into their support structures for two limiting cases: supports that can be treated as plates, and supports that act as semi-infinite elastic media, with effectively infinite thickness. The former case is applicable to many microscale resonators, while the latter is appropriate for nanoscale devices. General formulations are given, applicable to a wide range of resonator geometries. These formulations are then applied to two geometries commonly used in microelectromechanical systems and nanelectromechanical systems applications: cantilevered beams and doubly fixed beams. Experimental data are presented to validate the finite-thickness support theory, and the predictions of the theory are also compared to data from existing literature for a microscale rectangular paddle oscillator.


Applied Physics Letters | 2003

Frequency entrainment for micromechanical oscillator

Maxim Zalalutdinov; Keith Aubin; Manoj Pandey; Alan T. Zehnder; Richard H. Rand; Harold G. Craighead; J. M. Parpia; Brian H. Houston

We demonstrate synchronization of laser-induced self-sustained vibrations of radio-frequency micromechanical resonators by applying a small pilot signal either as an inertial drive at the natural frequency of the resonator or by modulating the stiffness of the oscillator at double the natural frequency. By sweeping the pilot signal frequency, we demonstrate that the entrainment zone is hysteretic and can be as wide as 4% of the natural frequency of the resonator, 400 times the 1/Q∼10−4 half-width of the resonant peak. Possible applications are discussed based on the wide range of frequency tuning and the power gain provided by the large amplitude of self-oscillations (controlled by a small pilot signal).


Journal of Applied Physics | 2005

A loss mechanism study of a very high Q silicon micromechanical oscillator

Xiao Liu; Joseph F. Vignola; H. J. Simpson; B. R. Lemon; Brian H. Houston; Douglas M. Photiadis

The room-temperature quality factors of silicon micromechanical oscillators have been investigated by scanning laser vibrometry. One of the flexural modes has very little attachment loss to its environment, which enables us to study internal loss mechanisms. After several consecutive annealing steps up to 800°C, the quality factor Q has increased from 8×104 to 6.0×105. However, the Q decays to 1.4×105 over six months in air. We conclude that near-surface lattice defects caused by reactive-ion etching and surface adsorbates are the main source of internal loss while surface adsorbates are responsible for the time dependence. We also discuss the thermoelastic limit in terms of Zener’s theory and flexural modal components of thin plates with vibratory volume change, and compare it with our results.

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J. A. Bucaro

Government of the United States of America

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Harry J. Simpson

Washington State University

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Douglas M. Photiadis

United States Naval Research Laboratory

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Maxim Zalalutdinov

United States Naval Research Laboratory

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Jeffrey W. Baldwin

United States Naval Research Laboratory

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Peter C. Herdic

United States Naval Research Laboratory

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Robert D. Corsaro

United States Naval Research Laboratory

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Earl G. Williams

United States Naval Research Laboratory

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Joseph F. Vignola

The Catholic University of America

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Martin H. Marcus

United States Naval Research Laboratory

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