#
U.S. Army Ballistic Research Laboratory
Resource Information
The organization ** U.S. Army Ballistic Research Laboratory** represents an institution, an association, or corporate body that is associated with resources found in **University of Oklahoma Libraries**.

The Resource
U.S. Army Ballistic Research Laboratory
Resource Information

The organization

**U.S. Army Ballistic Research Laboratory**represents an institution, an association, or corporate body that is associated with resources found in**University of Oklahoma Libraries**.- Label
- U.S. Army Ballistic Research Laboratory

## Context

Context of U.S. Army Ballistic Research Laboratory#### Contributor of

- BRL Report, no. 1142
- A computer program to calculate the physical properties of a system of coaxial bodies of revolution
- A device and technique for optically aligning a light beam relative to a reference axis
- A double-charge technique to measure face-on blast
- A fast acting diaphragm cutter
- A high stiffness electromagnetic weighing system
- A high stiffness electromagnetic weighing system
- A limited aerodynamic test of the 2 1/2-inch ring airfoil grenade (RAG-A)
- A method for obtaining aerodynamic coefficients from yawsonde and radar data
- A miniature flush-mounted tourmaline gauge
- A modified least squares reduction technique for interferograms
- A multiple mercury manometer read by the capacitive method
- A nonsimilar moving wall boundary layer problem
- A plastic-rigid theory of the response of beams to air blast loading
- A precision yawsonde calibration technique
- A solution for laminar flow past rotating cylinder in crossflow
- A statistical comparison of two methods of interferogram reduction
- A study of artillery shell drift at high angle of fire using solar aspect sensors
- A study of the vibrations of shallow spherical shells
- A transient experiment using a multiple-pulse laser light source
- Additional two-dimensional wake and jet-like flows
- Advances in the dynamic analysis of range data
- Aerodynamic data for small arms projectiles
- Aerodynamic derivatives for both steady and non-steady motion of slender bodies
- Aerodynamic properties of 4.9-calibers long, square based shell at transonic speeds
- Aerodynamic properties of a 105mm model of the 8" T347E1 shell
- Aerodynamic properties of a caliber 0.50 bullet with reflex boattail
- Aerodynamic properties of the 2.75-inch rocket T131
- Aerodynamics of sabot discard within a muzzle blast environment
- Air blast loading on three-dimensional scale models of a semi-cylinder
- Air blast measurements around water-filled simulated nuclear reactor core vessels
- An X-ray analysis of the strain in steel due to impulsive loads
- An elementary review of the Mathieu-Hill equation of real variable based on numerical solutions
- An exact re-statement of the equations of motion of a rigid projectile for use with modern computing machinery
- An expansion of tables II and III of N.A.C.A. TN no. 1428
- An experimental study of data capsule ejection through a nose-cone trailing wake
- An integral analysis of boundary layers on moving walls
- An integrated environment for army, navy and air force target description support
- An interesting sabot design
- Analog computer simulation of flight characteristics of two 90mm fin stabilized shell T108E40 and T316
- Analysis of mechanical and gasdynamic loadings during sabot discard from gun launched projectiles
- Apparatus for study of fluid motion in a spinning cylinder
- Automated estimation of kinetic rate parameters and mechanism of complex gas-phase chemical reactions
- BRL : U.S. Army Ballistic Research Laboratories, Aberdeen Proving Ground, Maryland
- Ballistic Research Laboratories' wind tunnel compressor plant
- Base pressure measurements on sharp and blunt 9Â° cones at Mach numbers from 3.50 to 9.20
- Boundary layer studies on a spinning cone
- Boundary layer studies on a spinning tangent-oglive-cylinder model
- Boundary layer transition on the NOL standard cone in the Ballistic Research Laboratories' supersonic wind tunnels
- Boundary-layer studies on spinning bodies of revolution
- Bounds on errors in KD caused by random errors of measurement in a five station range
- Calculated peak pressure-distance curves for Pentolite and TNT
- Calculation of the velocity profiles of the incompressible laminar boundary layer on a yawed spinning cone and the magnus effect
- Chapman-Kirk reduction of free-flight range data to obtain nonlinear aerodynamic coefficients
- Characteristic calculation of non-equilibrium flows
- Characteristics of the sidewall and floor boundary layers in BRL supersonic wind tunnel no. 1
- Chronograph error in drag measurements
- Comments on the effect of punched and lain fuze covers on the aerodynamic properties of the 90-MM T91E1 shell at M=1.2
- Comments on the use of guns to launch high altitude probes
- Comparative evaluation of the 20mm developmental ammunition - exterior ballistics
- Comparison of the performance of candidate muzzle devices for 30 mm cannon
- Composite V/STOL utility/logistics aircraft, speed versus payload and productivity
- Compressible turbulent boundary layer computations for flow with longitudinal curvature
- Computation of sabot discard
- Computation of the transonic flow over a wedge with detached shock wave by the method of steepest descent
- Computational implications of the zone of dependence concept for three-dimensional boundary layers on a spinning body
- Contributions of a wall shear stress to the Magnus effect on nose shapes
- Cooling water system, compressor plant no. 1
- Correction of non-linearity in electromagnetic weighing devices
- Correlation parameters for two-dimensional jet interaction
- Data reduction of the yaw and swerve of a fin-stabilized missile with a roll varying through resonance for a high speed electronic digital computer
- Degraded states vulnerability analysis, Phase II
- Derivation of equations for the stresses and strains in a cylindrical viscoelastic case-bonded grain
- Description of a Fortran program DAWNA for analysis of muzzle blast field
- Drag and dispersion of banded spheres with and without stings
- Dynamics of liquid-filled shell : aids for designers: a) Milne's graph, b) Stewartson's tables
- Effect of Magnus torque on the yaw damping of the 90-mm T108E46 shell
- Effect of a hemispherical base on the aerodynamic characteristics of shell
- Effect of large high-frequency angular motion of a shell on the anaylsis of its yawsonde records
- Effect of spin on aerodynamic properties of bodies of revolution
- Effectiveness of lining materials in increasing the blast resistance of a simulated outer containment vessel for a nuclear reactor
- Elastic response to blast loading of strain-rate dependent cantilevers
- Estimation of the static aerodynamic characteristics of ordnance projectiles at supersonic speeds
- Evaluation of the computer codes BLAST, DORF, HELP and HEMP for suitability of underexpanded jet flow calculation
- Expansion waves in metals vaporized by electron beam pulses
- Expected coverage of a circular target with a salvo of N area-kill weapons
- Experimental verification of the inertial oscillations of a fluid in a cylinder during spin-up
- Experiments on wake optical properties
- Exploding wire light source for high speed interferometry
- Ferromagnetic core logical circuitry and its application to digital computers
- Flame spreading in small arms ball propellant
- Fluctuation measurements in supersonic turbulent boundary layers
- Free oscillations of liquid during spin-up
- Free radicals : bibliography and survey of publications, up to 1959
- Fringes with heterochromatic light
- Full-scale free-flight ballistic measurements of guided missiles
- Gravity-induced angular motion of a spinning missile
- Growth of the turbulent inner wake behind large spheres at supersonic velocities
- Growth of the turbulent wake behind a supersonic sphere
- High-speed computing machine calculation of supersonic axisymmetric flows
- High-strength uranium-0-8 weight percent titanium alloy penetrators
- Hot-wire measurements in a cylinder wake for low Reynolds number flow at Mach two
- Hypervelocity impact by collision of two projectiles :, Phase II
- Hypervelocity impact phenomena : preliminary background report, November 1961
- Hypervelocity micro-particle impact on thin foils
- IBGRAF : display of XNOVAKTC interior ballistic computations
- In-flight payload temperature measurements for the XM736 binary projectile
- Index of refraction of excited monatomic gases
- Inertial properties of symmetric sabot components
- Initial heating rates and energy inputs for exploding wires
- Instrumentation of structures for air-blast and ground-shock effects
- Interferometry in the far UV : photometric aspects
- Interim report on projectile, 155mm: HE, XM549
- Laser doppler shift velocimeter
- Laser interferometry of unsteady, underexpaned jets
- Launch dynamics of a single flechette round
- Laws for large elastic response and permanent deformation of model structures subjected to blast loading
- Magnetic spin accelerator
- Magnus effect in the case of rotating cylinders and shell
- Measurement of air blast effects from simulated nuclear reactor core excursions
- Measurement of electron concentrations in an axisymmetric nonequilibrium shock layer
- Measurement of frequency response of pressure gauges by a high-pressure shock tube technique
- Measurement of spin decay and instability of liquid-filled projectiles via telemetry
- Measurements of payload temperature on-board the XM687 155mm binary projectile
- Miniature piezoelectric gages for measuring transient pressures on airfoils
- Monochromatic light source for interferometry of high-speed gas flows
- Muzzle blast flow field calculations
- Muzzle devices, a state-of-the-art survey :, Volume I, Hardware study
- Note on shock reflection coefficient
- Numerical experiments to integrate the Navier-Stokes equations
- Observations of the deformation of aluminum subjected to impulsive loads of constant maximum amplitude and variable impulse
- On resonance phenomena and short ranges in mortar fire
- On the free flight drag determination of a finned configuration (RM-10) flying at critical Reynolds numbers
- On the quasi-linear substitution method for missile motion caused by strongly nonlinear static moment
- On the use of vacuum ultraviolet absorption as a measure of temperature in rare gas plasmas
- On-board projectile measurements for exterior ballistics
- Parametric sensitivity study of a numerical model for flame spreading
- Penetration of shaped-charge jets into glass and crystalline quartz
- Planar limit motion of nonspinning symmetric missiles acted on by cubic aerodynamic moments
- Potential energy of yaw in static case
- Preliminary radiation measurements of high speed flows over cylinders and spheres
- Preliminary report on medium studies
- Preliminary results obtained with catalytic surfaces in the upper atmosphere during balloon flights : upper atmosphere research report no. III
- Preliminary surveys of the three dimensional boundary layer on a yawed, spinning body of revolution
- Preparation of the BRL tank car torch facility at the DOT, Transportation Test Center, Pueblo, Colorado
- Projectile high-g telemetry for long range dynamics measurements
- Quick methods for estimating the static aerodynamic coefficients of shell
- RECRIF users' manual
- Reflected shock initiation of a chemical reaction
- Refraction operators and ray tracing through cones of constant index
- Resonant thermal-acoustic oscillations
- Response of an asymmetric missile to spin varying through resonance
- Response of submerged spherical shells to internal blast loading
- Sabot aerodynamics during discard
- Self-aligning rockets
- Shock pressures in tunnels oriented face-on and side-on to a long duration blast wave
- Shock tube pulse shaper
- Shock tube pulse shaper
- Shock-wave yaw for 9 1/2Â° semi-apex cone
- Similarity solution of the boundary layer equations for flow over a moving wall
- Simultaneous streak and frame interferometry for use in short duration hypervelocity facilities
- Solutions of reaction rate equations pertaining to electron irradiation of 4:1 mixtures of N2 and O2
- Some aerodynamic effects of blunting a projectile nose
- Some aerodynamic effects of varying the body length and head length of a spinning projectile
- Some aerodynamic properties of a 105mm model of the 155mm T-358 shell
- Some aerodynamic properties of three 105mm shell, M1, T377 and T107
- Some applications of gradient methods
- Some experiments with liquid-filled, impulsively started, spinning cylinder
- Spiral yawing motions of 81mm M56 shell : a study in non-linear theory
- Stability and transport characteristics of flames
- Stability characteristics as determined by yaw card measurements for four 20mm projectiles for the VRFWS-I ; HEIT M599, HEIT XM706, TPT M206, TPT M206E2
- Stress function theory for linearly viscoelastic solids
- Stress waves through projectile joints and interfaces
- Studies of the deformation mechanics of an impulsively loaded copper single crystal
- Study of hypervelocity micro-particle cratering
- Subsurface accelerations and strains from an underground detonation, Part II
- Supersonic drag and base pressure of a 70Â° cone cylinder
- Survey spectra of a pinched argon plasma
- Tables of cylindrical blast functions for [gamma] : 5/3 and [gamma] = 7/5
- Tables of the first 200 factorials to 20 places
- Techniques for fabricating fast response heat transfer gages
- The B-H6 tube light source for interferometry
- The aerodynamic properties of a spike-nosed shell at transonic velocities
- The aerodynamic properties of the 105mm HE shell, MI, in subsonic and transonic flight
- The axisymmetric modes of vibration of thin spherical shell
- The comparison of strain and kinetic energy in a plastic wave moving through sand
- The design of a second generation yawsonde
- The drag and stability of a circular wedge airfoil in supersonic flight
- The drag and stability properties of the hemispherical base shell, 75mm, T50E2
- The drag properties of several winged and finned cone-cylinder models
- The dynamic properties of pure cones and cone cylinders
- The dynamical effect of inertial waves on the free flight motion of a body containing several eccentrically located, liquid-filled cylinders
- The effect of a rotating band upon some aerodynamic coefficients of the seven-caliber Army-Navy spinner rocket at Mach 1.8
- The effect of boattailing on the drag coefficient of cone-cylinder projectiles at supersonic velocities
- The effect of muzzle device configuration on the blast overpressure levels on the AH-1S helicopter tow sight unit
- The effect of muzzle jet asymmetry on projectile motion
- The effects of Reynolds number, Mach number, spin rate, and other variables on the aerodynamics of spheres at subsonic and transonic velocities
- The effects of alpha particles on low density polyethylene
- The effects of annular rings and grooves, and of body undercuts on the aerodynamic properties of a cone-cylinder projectile at M : 1.72
- The effects of steady, three-dimensional perturbations in boundary layers
- The elastic response of thin spherical shells to internal blast from eccentrically placed explosive charges
- The elastic response to internal blast loading of models of outer containment structures for nuclear reactors
- The elastic-plastic response of thin spherical shells to internal blast loading
- The flow field about the muzzle of an M-16 rifle
- The generation and propagation of seismic energy from a buried explosive source
- The generation and propagation of seismic energy from a buried explosive source
- The high-speed flexible-throat supersonic wind tunnel
- The inertial wave frequency spectrum in a cylindrically confined, inviscid, incompressible, two component liquid
- The marriage of optical, tracer and surface indicator techniques in flow visualization
- The numerical solution of Laplace's equation on ORDVAC
- The numerical solution of non-linear differential equations by the method of steepest descent
- The plastic response to internal blast loading of models of outer containment structures for nuclear reactors
- The pressure distributions about 60mm and 81mm mortar projectiles during shot ejection
- The response of cylindrical shells to external blast loading
- The response of cylindrical shells to external blast loading, Part II
- The response of elastic spherical shells to spherically symmetric internal blast loading
- The response of simple beams with a central mass to a constant force applied instantaneously at the center
- The role of the zone of dependence concept in three-dimensional boundary-layer calculations
- The singular nature of three-dimensional perturbations of boundary layers and the small cross flow theory
- The structure of three-dimensional separated flows in obstacle-boundary layer interactions
- The subsonic aerodynamic characteristics of the 105mm HE shell, M1 at angles of attack from zero to 180 degrees
- The yawing of a projectile whose moment changes sign
- Theoretical basis of the recoilless rifle interior ballistics code "RECRIF"
- Theoretical temperature distribution in the precursor region ahead of projectiles traveling at hypersonic velocities
- Three dimensional flow studies over a spinning cone at angle of attack
- Trajectory models in mortar fire
- Turbulent boundary layers in blast wave and shock tube flows
- Two machine methods for determination of eigenvalues and eigenvectors of real symmetric matrices
- Two numerical methods for calculating axisymmetric flow
- Two wavelength, streak interferometry of an ionized, heavy gas
- Universal curves for spin histories of vacuum trajectories
- Vacuum ultraviolet radiation in the expansion tube
- Verification of ground test data by instrumented flight test of an artillery shell
- Visualization of cylindrical shock waves
- Vulnerability Lethality Division
- Vulnerability/Lethality Division armed for the 90's and beyond
- Wall heat transfer effects on supersonic nozzle wall boundary-layer temperature profiles
- Wind tunnel force tests of Saturn V configurations at supersonic Mach numbers
- Wind tunnel force tests of a Mercury Redstone configuration, without escape rocket pylon, at supersonic Mach numbers
- Wind tunnel magnus testing of a canted fin or self-rotating configuration
- Wind tunnel supply headers
- Wind tunnel testing facilities at the Ballistic Research Laboratories
- Wind tunnel tests of rectangular finned variable gap tangent ogive-cylinder model at Mach numbers 1.75 to 4.50
- Wind tunnel tests of the Redstone "B" nose cone at Mach numbers from 1.75 to 5.00

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