Eric J. Jumper's research while affiliated with University of Notre Dame and other places

Publications (288)

Article
Experimental Shack-Hartmann wavefront sensor (SHWFS) measurements were collected for a laser beam that propagated through a weakly compressible shear layer. Complementary computational fluid dynamics (CFD) was also conducted to match the experiment. The path-integrated CFD results were then applied to a SHWFS model such that the experimental and CF...
Book
Aero-Optical Effects: Physics, Analysis and Mitigation delivers a detailed and insightful introduction to aero-optics and fully describes the current understanding of the physical causes of aero-optical effects from turbulent flows at different speeds. In addition to presenting a thorough discussion of instrumentation, data reduction, and data anal...
Chapter
This chapter discusses the effect of the finite aperture size on the measured wavefronts. Specifically, it discusses the aperture effect on the global tip/tilt and the higher‐order wavefront distortions. Z‐tilt definition is used to define the global tip/tilt. Transfer functions, relating the local deflection angle and the global tip/tilt, and the...
Chapter
This chapter reviews several commonly used experimental techniques for measuring optical distortions imposed on a wavefront of a collimated beam. It includes interferometry technique, wavefront curvature methods, and gradient‐based wavefront sensors. The last category of sensors is discussed in more details, including a detailed discussion of Shack...
Chapter
This chapter discusses experimental studies of aero‐optical component of beam jitter. Various contaminations of aero‐optical beam jitter in typical tunnel environment, like mechanically induced jitter, and possible means to remove them from the data are discussed. A newly developed stitching method, which provides robust means of extracting aero‐op...
Chapter
This chapter gives a minimal background in optics to understand the aero‐optics material to follow in later chapters. A definition of wavefront distortions and related local deflection angles is introduced, and their components and quantitative ways to characterize them are discussed. The linking equation is introduced and discussed, which provides...
Chapter
In this chapter the limits to compensation of aero‐optical wavefront disturbances through use of adaptive optics (AO) techniques is quantified. An outline of the key temporal and spatial statistics of aero‐optical disturbances which govern the capability of AO compensation are given. It is shown that the temporal spectrum of aero‐optical disturbanc...
Chapter
This chapter discusses mitigation of aero‐optic effects. The topic is divided into flow control and adaptive optics. In particular, it focusing primarily on how the material in the rest of the book applies to an adaptive optics system. The components in a beam control system are introduced and how each applies to the various characteristics of aero...
Chapter
This chapter presents and discusses aero‐optical distortions due to typical turbulent flows, like shear layers, boundary layers, and flows around commonly used side‐mounted turrets. First, it introduces useful scaling laws, which allows re‐scaling of aero‐optical distortions to different flow regimes and speeds. Physical mechanisms and semi‐empiric...
Chapter
This chapter introduces some of the common methods that have been used in the aero‐optical community over the last two decades. Each of the methods makes use of specific approaches and principles developed to overcome some of the contamination that is always present in the optical data. The methods are grouped into several major categories. Statist...
Article
Full-text available
In this paper, atmospheric optical turbulence strength is estimated for realistic airborne environments using a modified phase-variance approach, as well as a modified slope-discrepancy approach. Realistic airborne environments are generated using wave-optics simulations of a plane wave propagating through increasing strengths of homogeneous atmosp...
Article
View Video Presentation: https://doi.org/10.2514/6.2022-3264.vid This paper presents the results of Mie scattering experiments in which a novel method is used to establish a relationship between scattered light intensity and flow field temperature. The results shown are for a weakly-compressible shear layer with high- and low-speed Mach numbers of...
Article
Full-text available
The work presented here experimentally measures the tilt imposed on a laser beam by the atmosphere from Shack–Hartmann wavefront sensor measurements collected in-flight. Tip/tilt is imposed on the laser beam by propagating through optical turbulent structures larger than or of the order of the size of the beam diameter. This tip/tilt causes a dynam...
Conference Paper
View Video Presentation: https://doi.org/10.2514/6.2022-0987.vid A simple acoustic mode-marching method is used to determine the acoustic environment of a wind-tunnel test-section assuming that the primary noise source is the wind-tunnel fan. In order to account for the change in cross-sectional shape from the circular fan duct to the square duct o...
Conference Paper
Full-text available
View Video Presentation: https://doi.org/10.2514/6.2022-0829.vid Wavefront measurements were collected from a laser beam which propagated between two aircraft at varying altitudes and separations. Various data processing procedures were employed for decoupling distortions imposed by the atmosphere and distortions imposed by the aero-optical environ...
Conference Paper
View Video Presentation: https://doi.org/10.2514/6.2021-2927.vid The flow over a surface can be effectively controlled using vertical fences that expand or contract in the cross-stream direction to slow or accelerate the flow as required. This passive flow-control approach, called the “virtual duct” was originally developed to mitigate aerooptical...
Article
Full-text available
A series of flight experiments have demonstrated a novel approach to measuring path-resolved optical turbulence quantities, such as Cn2, along an air-to-ground slant path. This paper describes the data acquisition experiments that involved two laser beams propagating between an orbiting airborne platform and a stationary ground terminal over an 8 k...
Article
Full-text available
While optical aberrations caused by atmospheric turbulence have been extensively investigated and well characterized, recent research has identified structural differences in optical phase distortions caused by aircraft-induced, compressible turbulence. These so-called aero-optical distortions can be a critical obstacle in the development of airbor...
Conference Paper
Full-text available
AAOL-BC was employed to conduct experiments which sought to measure atmospheric induced jitter on a laser beam. Wavefronts were collected for a laser beam which was propagated between two aircraft at varying altitudes and separations. A data processing procedure for extracting the turbulence induced jitter is presented and the resulting jitter and...
Article
Experimental studies of the changes in turbulence characteristics inside a boundary layer due to external forcing were performed using hot-wire anemometry. The forcing was created by a periodically forced shear layer that was external to a compressible subsonic turbulent boundary layer. The convecting coherent structures in the shear layer create a...
Conference Paper
Experimental studies of the changes in turbulence characteristics inside a boundary layer due to external forcing were performed using hot-wire anemometry. The forcing was created by a periodically forced shear layer that was external to a compressible subsonic turbulent boundary layer. The convecting coherent structures in the shear layer create a...
Article
Full-text available
Optical distortions caused by turbulent airflow surrounding an aircraft, known as aero-optical phenomena, are a major impediment to applications of airborne laser systems. To better understand the spectral properties of aero-optical distortions, a general expression for the wavenumber spectrum of the refractive index is derived from the ideal-gas l...
Article
Wavefront measurements were performed in-flight for a hemispherical turret on the Airborne Aero-Optics Laboratory-Transonic (AAOL-T). For turret side-looking angles near 90 deg, upstream-propagating optical distortions over the turret aperture were observed. These distortions were contributed to acoustic waves originating from the engine downstream...
Article
The aero-optical effect of a flat-plate adiabatic boundary layer has been measured using the light generated by a laser-induced breakdown spark. The measurements were performed in a blowdown wind tunnel at freestream Mach numbers of 3 and 4.38. The tests showed that the aero-optical effect of boundary layers with rms optical path difference as low...
Article
Full-text available
The aero-optical environment around a hemisphere-on-cylinder turret with both flat and conformal windows was studied experimentally in flight using the Airborne Aero-Optical Laboratory-Transonic for a range of subsonic and transonic Mach numbers between 0.5 and 0.8. Above M = 0.6 , the local shock appeared near the top of the turret, causing additi...
Article
Full-text available
The field of aero-optics is devoted to the study of the effects of turbulent flow fields on laser beams projected from airborne laser systems. This article reviews the early and present periods of research in aero-optics. Both periods generated impressive amounts of research activity; however, the types and amount of data differ greatly in accuracy...
Article
Methods and results are described for flight-test measurements of the aero-optical effect of the near-field flow surrounding a medium-sized helicopter in hover. The data were acquired using a novel, passive measurement approach in which optical wave-front aberrations were computed from the displacements of light-emitting diodes attached to a target...
Conference Paper
This paper describes an experiment in which a forced shear layer external to a turbulent boundary layer is used to impart external large-scale forcing to the boundary layer. The shear-layer forcing creates periodic coherent vortical structures in the shear layer that convect at the shear-layer convective velocity. The convecting coherent structures...
Conference Paper
by optical tracking of the light emitted by a laser-induced breakdown (LIB) spark is described. The measurements were performed in a blowdown wind tunnel at a nominal flow Mach number of 4.38. The tests showed that flow velocity could be accurately measured using the technique, with a demonstrated flow-angle uncertainty of less than ± 0.2 o at the...
Article
Full-text available
This paper presents experimental studies of aero-optical distortions due to a turbulent boundary layer over a range of subsonic speeds with the underlying wall both heated above and cooled below the adiabatic wall temperature. A statistical scaling model, based on extended strong Reynolds analogy is derived and shown to correctly predict experiment...
Conference Paper
Full-text available
The aero-optical characteristics of the wake beneath a hovering helicopter was computed using Unsteady RANS (URANS) and Large-Eddy Simulations (LES). The computational methodology consisted of combining a URANS simulation with a vorticity-confinement method to produce a model of the large-scale vortex wake of the helicopter. An LES simulation of th...
Article
A fast low-order computational approach is presented for estimating the aero-optic effect of the rotor tip vortex system on helicopter-borne optical systems. The approach employs prescribed-wake methods that have been developed by the helicopter design community to rapidly generate realistic approximations to the vortex-wake systems of helicopters...
Conference Paper
A new data-driven method for latency compensation in adaptive optics sytems is developed and evaluated in this paper. Conventional adaptive optic controllers typically assume a single timestep of latency in the feedback loop, which is an appropriate assumption for low-frequency applications such as atmospheric optics compensation. However, the cont...
Article
A comparison between the spatial and temporal requirements for designing adaptive-optic correction systems for aero-optical turbulence over the pupil of a turret on the side of an airborne platform is presented. These systems are necessary to mitigate the deleterious aero-optic effects on an optical beam and to reopen the field of regard. The deriv...
Conference Paper
Full-text available
Extensive studies of the local shock dynamics in transonic compressible flow near partially-protruding cylindrical turret are presented and discussed. Spatially-temporally resolved wavefront measurements with a high-speed Shack-Hartmann sensor, synchronized with high-speed shadowgraph system and unsteady pressure measurements on the turret surface...
Conference Paper
Wavefront measurements of a turbulent boundary layer were performed at the University of Notre Dame. Optical access windows to the tunnel were instrumented with 16 accelerometers to measure the tunnel-induced vibrations in the optical windows. A combination of spectral Proper Orthogonal Decomposition (POD) and Linear Stochastic Estimation (LSE) wer...
Article
Full-text available
This paper gives the most-complete characterization to date of the optical aberrations imposed on a laser beam propagated through a subsonic, compressible, turbulent boundary layer in a zero-pressure gradient environment, over a range of boundarylayer thicknesses, oblique propagation angles and Mach numbers. This characterization is based on optica...
Conference Paper
Using large eddy simulation, Mach 0.4 flow over a hemisphere-on-cylinder turret is simulated to investigate the aero-optical effects caused by turbulent density fluctuations. The height of the cylinder is 0.375 times the hemisphere diameter and the Reynolds number based on the turret diameter and free stream velocity is 460,000. Comparisons are mad...
Conference Paper
Simultaneous point surface pressure measurements, accelerometer, optical wavefront and jitter measurements were performed using a hemisphere-on-cylinder turret with realistic geometric features like "smiles" at M = 0.33 and M = 0.4. A Linear Stochastic Estimation (LSE) technique was used to separate the aero-optical and the aero-mechanical jitter c...
Conference Paper
In this paper we present two algorithms for estimating the aero-optical aberration of a transonic flow around a 2-D turret based on Malley probe signals or pressure signals from a few selected points. These two algorithms use Artificial Neural Networks and Linear Stochastic Estimation of varying model orders to estimate Proper Orthogonal Decomposit...
Article
Spatially temporally resolved unsteady pressure fields on a surface of a hemisphere-on-cylinder turret with either a flat or a conformal window with realistic features such as gaps and ‘‘smile’’ cutouts were characterized using fast-response pressure-sensitive paint at M = 0.33 for several window viewing angles. Various statistical properties of pr...
Article
An alternative adaptive-optic controller, using both flow control and a phase-lock-loop control strategy, has been designed to overcome bandwidth limitations inhibiting current adaptive-optic controllers. Adiscrete-vortex code and weakly compressible model were used to simulate high-speed shear layer adaptive-optic corrections based upon the propos...
Article
Recent in-flight aero-optical measurements from the Airborne Aero-Optics Laboratory are provided, along with instrumentation and experimental set-up. Results of an extensive survey of the aero-optical environment at different viewing angles, for both flat-window and conformal- window turrets at different subsonic and low transonic speeds below M =...
Article
In-flight wavefront measurements around a flat-window turret at subsonic Mach numbers are analyzed in instantaneous and timeaveraged sense. In addition to the root-mean-squared levels of aerooptical distortions, higher-order spatial statistics are calculated, and their dependence as a function of the viewing angle is discussed. Given the optical da...
Conference Paper
Fast-response pressure-sensitive paint (PSP) was used in this work for a study of the unsteady surface pressures resulting from the complex separated flow over a hemispherical turret model. The turret includes several distinct features such as a flat window and crevices that are based on functional requirements, but also introduce interesting addit...
Conference Paper
Spatially-temporally-resolved unsteady pressure fields on a surface of a hemisphere-on-cylinder turret with either a flat- or a conformal-window were characterized using fast-response pressure sensitive paint at M = 0.33 for several window viewing angles. Various statistical properties of pressure fields were computed and geometry effects on unstea...
Conference Paper
Full-text available
The methodology and results of a computational investigation into the nearfield aerooptic effects on a helicopter-borne optical system are presented. The approach investigated in the study was to incorporate a vorticity-confinement method into a commerciallyavailable CFD code, thereby allowing the rotor wake to be modeled in a less computationally-...
Conference Paper
Aero-optical mitigation effect of a passive flow control device consisted of a pair of delta-wing vortex generators placed on both sides near a hemisphere-on-cylinder turret was experimentally studied in-flight aboard the Airborne Aero-Optics Laboratory (AAOL) at different subsonic speeds. The optical environment was characterized with a 2D high sp...
Conference Paper
The spatially-temporally-resolved pressure field on a surface of a hemisphere-on-cylinder optical turret was characterized in a wind tunnel at M = 0.33 using fast-response Pressure Sensitive Paint (PSP), simultaneously with 8 pressure sensors. A sparse unsteady pressure field was also obtained in-flight for subsonic speeds of M = 0.5 on the Airborn...
Article
This paper discusses the aero-optical environment for a flat-window hemisphere-on-cylinder turret over a wide range of viewing angles during flight tests in the Airborne Aero-Optics Laboratory. Aero-optical aberrations around the turret were measured using a high-speed Shack-Hartmann wave-front sensor providing an extensive aero-optical mapping. Th...
Article
Spherical turrets are effective platforms for integrating optical systems into aircraft because they are able to aim the optical system over a large field of regard without altering their basic aerodynamic shape. The spherical turret shape is susceptible, however, to flow separation from its leeward surface. At compressible flowspeeds, the shear la...
Article
Full-text available
The mitigation of aero-optical aberrations in the wake of a surface-mounted turret comprised of a hemisphere mounted on a matching cylindrical support is investigated in wind tunnel experiments. The effects of hybrid (passive/active) flow control on the aero-optical and aerodynamic characteristics of the flow over a conformal optical aperture embed...
Conference Paper
The mitigation of aero-optical aberrations in the wake of a surface-mounted turret comprised of a hemisphere mounted on a matching cylindrical support is investigated in wind tunnel experiments. The effects of hybrid (passive/active) flow control on the aero-optical and aerodynamic characteristics of the flow over a conformal optical aperture embed...
Conference Paper
Aero-optical effects around the hemispheric turret at forward looking angles for azimuthal angles of 0°, 45° and 85° at the elevation angle of 45° were parametrically investigated for multiple turret geometries and flow conditions. 2D wavefronts were acquired with a 32×32 sub-aperture resolution at 25 kHz with global beam jitter and accelerometer m...
Conference Paper
Experimental studies of the aero-optical effects around a partially-protruding cylindrical turret for a range of incoming transonic Mach numbers are presented and discussed. Spatially-temporally resolved wavefronts were collected using a high-speed Shack-Hartmann sensor and flow visualization was performed with a Schlieren system. Different flow re...
Conference Paper
When a laser beam is transmitted from an airborne platform, it must first pass through a relatively thin region of the turbulent flow in the immediate vicinity of the airplane. Unsteady density variations present in the turbulent flow will imprint spatial/temporal variations on the otherwise planar outgoing wavefronts. These variations in wavefront...
Article
A method for extracting the convection speed and direction of aberrations present in wavefronts due to aero-optical turbulence over the pupil of a turret on the side of an airborne platform is addressed. The method is applied to data from the Airborne Aero-Optics Laboratory (AAOL). Such convection information is useful in designing feed-forward ada...

Citations

... In order to better understand the underlying physics associated with these aero-optical aberrations, extensive lab-based [2][3][4][5]7,8,[14][15][16][17][18][19][20][21] and aircraft-based 6,[22][23][24][25][26][27][28][29][30] testing has been conducted in recent years. Although many foundational aero-optical experiments and analyses have been conducted, there is still much to learn about the coupling of fluidic properties and optical aberrations. ...
... Shack-Hartmann wavefront sensors are commonly used to measure the aero-optical distortions caused by the dependence of the air index of refraction on the gas density, as quantified by the optical path difference (OPD), in subsonic flow [28] atmospheric studies [29], as well as supersonic/hypersonic flows [30]. Since a Shack-Hartmann sensor measures the line-of-sight integral of fluctuations in the index of refraction caused by density inhomogeneity in the flow, it is used in this study to augment the qualitative schlieren imaging method in a horizontal plane, including a local flow velocity estimate, and provide an initial analysis of the flow perturbation pattern in the cross-flow direction, orthogonal to the pins-related shear layer. ...
... By leveraging the frozen turbulence hypothesis, measurement of the refractive index power spectral density (PSD) can be done optically through various methods such as wavefront sensing [6], differential seeing monitors [7], and optical phase noise [8][9][10]. The measurement of the optical phase noise has been of interest due to its use for determining the phase noise present in a communication system; however, it can also be used for sensing as the timing phase noise PSD, which is directly related to the refractive index PSD. ...
... In the aero-optical community, remarkable progress has been witnessed using wind tunnel experiments. Kemnetz et al. 30 tested the wavefront phase change induced by a Ma j (the subscript denotes jet) 0.07 injection emanating into an ambient Ma 1 0.6 flow, and employed a sub-harmonic disturbance for aero-optical control. From their observations, modifying the pressure-velocity term in strong Reynolds analogy (SRA) analysis was found to promote the accuracy of aero-optical estimation. ...
... Laser-based applications in the atmosphere or ocean, such as imaging [1], free-space communications [2], sensing [3], or directed energy [4], are subject to random density changes of the fluid due to turbulence. These random density changes vary the medium's refractive index, which affects light propagation by creating fluctuations in the optical path length and, consequently, the optical phase. ...
... A wide field of view (WFOV) camera with a 300 [mm] lens was used to locate the laboratory aircraft, and a narrow field of view (NFOV) camera with a 600 [mm] lens was used for tracking-either off the return signal or image features on the laboratory aircraft. Using the motorized beam divergence system, the divergence of the outgoing beam was changed by the user to sufficiently fill the acquisition window on the laboratory aircraft window regardless of the separation distance between aircraft [19,20]. ...
... The protrusion of the turret into the freestream flow creates a complicated turbulence environment, which can degrade the performance of these optical systems. [1][2][3][4][5][6][7][8][9][10] The optical-turbulence environment, which is caused by aerodynamic turbulence, is colloquially referred to as aero optics. [11][12][13] Laser beam propagation through shear layers has been one aero-optical environment of particular interest. ...
... The protrusion of the turret into the freestream flow creates a complicated turbulence environment, which can degrade the performance of these optical systems. [1][2][3][4][5][6][7][8][9][10] The optical-turbulence environment, which is caused by aerodynamic turbulence, is colloquially referred to as aero optics. [11][12][13] Laser beam propagation through shear layers has been one aero-optical environment of particular interest. ...
... In order to better understand the underlying physics associated with these aero-optical aberrations, extensive lab-based [2][3][4][5]7,8,[14][15][16][17][18][19][20][21] and aircraft-based 6,[22][23][24][25][26][27][28][29][30] testing has been conducted in recent years. Although many foundational aero-optical experiments and analyses have been conducted, there is still much to learn about the coupling of fluidic properties and optical aberrations. ...
... As early as the 18th century, astronomers recognized the limitations imposed on stellar observations by the influence of the atmosphere, which is because the components in the atmosphere are not uniformly distributed most of the time, leading to various aberrations [1,2] brought about by the inhomogeneity of the atmospheric refractive index in time and space [3]. Nowadays, especially with the rapid development of optical technology, researchers have further realized the impact of atmospheric refraction on related fields, leading to a deeper study of atmospheric refraction. ...