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Charts, diagrams, etc
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The concept ** Charts, diagrams, etc** represents the subject, aboutness, idea or notion of resources found in **University of Oklahoma Libraries**.

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Charts, diagrams, etc
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The concept

**Charts, diagrams, etc**represents the subject, aboutness, idea or notion of resources found in**University of Oklahoma Libraries**.- Label
- Charts, diagrams, etc

## Context

Context of Charts, diagrams, etc#### Subject of

- 1984 direct strike lightning data
- A buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with NACA 64A thickness distributions, fences, a leading-edge extension, and body contouring
- A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine - 2
- A flight and analytical study of methods for reducing automatic-interceptor tracking errors caused by target maneuvers
- A free-flight investigation of the effects of simulated sonic turbojet exhaust on the drag of a boattail body with various jet sizes from Mach number 0.87 to 1.50
- A guide to graph colouring : algorithms and applications
- A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver
- A study of liquid boric oxide particle growth rates in a gas stream from a simulated jet engine combustor
- A study of the effect of aftercooling on the power and the weight of a 2000-horsepower air-cooled engine installation
- A study of the response of panels to random acoustic excitation
- A summary of drag results from recent Langley full-scale-tunnel tests of Army and Navy airplanes
- A survey of methods for turbojet thrust measurement applicable to flight installation
- A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05
- A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion
- Acoustical treatment for the NACA 8- by 6-foot supersonic propulsion wind tunnel
- Additional power-on wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane with full-span slotted flaps
- Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4
- Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section : Transonic-bump method
- Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88
- Aerodynamic characteristics of a spoiler-slot-deflector control on a 45° sweptback wing at Mach numbers of 1.61 and 2.01
- Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section : Transonic-bump method
- Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds
- Aerodynamic investigation at Mach number 1.92 of a rectangular wing and tail and body configuration and Its components
- Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5
- Air-flow and performance characteristics of engine-stage supercharger of a double-row radial aircraft engine : 2 - Effect of design variables
- Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds
- An analog study of a shock-position diffuser control on a supersonic turbojet engine
- An approximate determination of the power required to move control surfaces as related to control-booster design
- An atlas of objectively analyzed atmospheric cross sections 1973-1980
- An atlas of upper tropospheric radiances observed in the 6 to 7 micrometer water vapor band using TOVS data from the NOAA weather satellites during 1979-1991
- An automated method for identifying inconsistencies within diagrammatic software requirements specifications : thesis ...
- An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds
- An inlet design concept to reduce flow distortion at angle of attack
- An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47° sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel
- An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2
- An investigation of the hydrodynamic characteristics of a dynamic model of a transonic seaplane design having a planing-tail hull
- Analytical evaluation of aerodynamic characteristics of turbines with nontwisted rotor blades
- Application of statistical theory to beam-rider guidance in the presence of noise, [Part] 2, Modified Wiener filter theory
- Approximate corrections for the effects of compressibility on the subsonic stability derivatives of swept wings
- Calculation of the aerodynamic loading of flexible wings of arbitrary plan form and stiffness
- Calculations of the performance of a compression-ignition engine-compressor turbine combination : 1 - Performance of a highly supercharged compression-ignition engine
- Calculations of the performance of a compression-ignition engine-compressor turbine combination, [Part] 2, Performance of complete combination
- Case in point : graph analysis for consulting and case interviews
- Characteristics of the Nike-Cajun (CAN) rocket system and flight investigation of its performance
- Charge-air distribution among the cylinders of a double-row radial aircraft engine
- Charts and approximate formulas for the estimation of aeroelastic effects on the lateral control of swept and unswept wings
- Charts and tables for use in calculations of downwash of wings of arbitrary plan form
- Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels
- Charts for calculation of the critical stress for local instability of columns with I-, Z-, channel, and rectangular-tube section
- Charts for estimating tail-rotor contribution to helicopter directional stability and control in low-speed flight
- Charts for estimation of the characteristics of a helicopter rotor in forward flight : 1 - Profile drag-lift ratio for untwisted rectangular blades
- Charts of pressure rise obtainable with airfoil-type axial-flow cooling fans
- Charts showing relations among primary aerodynamic variables for helicopter-performance estimation
- Charts showing stability and control characteristics of airplanes in flight
- Combustion efficiency and altitude operational limits of three liquid hydrocarbon fuels having high volumetric energy content in a J33 single combustion
- Combustion of aluminum borohydride in a supersonic wind tunnel
- Comparison of experimentally and analytically determined windmilling characteristics of a compressor with low over-all pressure ratio
- Correlation of flight and analog investigations of roll coupling
- Correlation of turbulent heat transfer in a tube for the dissociating system N204 reversibly yields 2N02
- Create Web Charts With jqPlot : display your data using innovative browser-based charts
- Create web charts with D3
- Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds
- Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress
- Determination of gas temperatures from the frequency of knock-induced gas vibrations in an internal-combustion engine
- Determination of the stability and control characteristics of airplanes from tests of powered models
- Diagram design : a constructive theory
- Diagram design : a constructive theory
- Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing
- Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades
- Effect of normal pressure on the critical compressive and shear stress of curved sheet
- Effect of normal pressure on the critical compressive stress of curved sheet
- Effect of propeller-axis angle of attack on thrust distribution over the propeller disk in relation to wake-survey measurement of thrust
- Effect of surface roughness on characteristics of spherical shock waves
- Effective data visualization : the right chart for the right data
- Effective data visualization : the right chart for the right data
- Effects of compressibility on maximum lift coefficients for six propeller airfoils
- Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds
- Effects of some external-store mounting arrangements and store shapes on the buffet and drag characteristics of wingless rocket-powered models at Mach numbers from 0.7 to 1.4
- Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds
- Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3
- Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds
- Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4
- Effects on adjacent surfaces from the firing of rocket jets
- Efficiency of a radial-flow exhaust-gas turbosupercharger turbine with a 12.75-inch tip diameter
- Elements of chart making,
- Equations and charts for the rapid estimation of hinge-moment and effectiveness parameters for trailing-edge controls having leading and trailing edges swept ahead of the Mach lines
- Evaluation of the use of electrical resistance for detecting overtemperatured S-816 turbine blades
- Examination of smoke and carbon from turbojet-engine combustors
- Excel 2013 for dummies analyzing & charting data course, Creating pivot charts
- Excel 2013 for dummies analyzing & charting data course, Customizing charts and chart elements
- Excel 2013 for dummies analyzing & charting data course, Editing the generic titles in a chart
- Excel 2013 for dummies analyzing & charting data course, Making professional-looking charts
- Excel 2013 for dummies analyzing & charting data course, Moving and resizing embedded charts
- Excel 2016 for dummies depicting data course, Adding explanatory text to a chart in Excel 2016
- Excel 2016 for dummies depicting data course, Creating charts with the Quick Analysis tool in Excel 2016
- Excel 2016 for dummies depicting data course, Creating pivot charts in Excel 2016
- Excel 2016 for dummies depicting data course, Creating sparkline graphs in Excel 2016
- Excel 2016 for dummies depicting data course, Customizing chart elements in Excel 2016
- Excel 2016 for dummies depicting data course, Editing the chart titles in Excel 2016
- Excel 2016 for dummies depicting data course, Inserting images in a chart in Excel 2016
- Excel 2016 for dummies depicting data course, Moving and resizing embedded charts in Excel 2016
- Excel 2016 for dummies depicting data course, Using the Ribbon to create a chart in Excel 2016
- Excel 2016 for dummies enhancing & sharing data course, Adding preset graphic shapes to a chart in Excel 2016
- Excel 2016 for dummies enhancing & sharing data course, Going fancy with SmartArt in Excel 2016
- Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination
- Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers
- Experimental investigation of the simulation of atmospheric entry of ballistic missiles
- Experimental pressure distributions over wing tips at Mach number 1.9, [Part] 2, Wing tip with subsonic trailing edge
- Factors affecting the maximum lift-drag ratio at high supersonic speeds
- Factors affecting transition at supersonic speeds
- Flight and analytical study of roll requirements of a fighter airplane
- Flight determination of drag and pressure recovery of two scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8
- Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8
- Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift
- Flight investigation of a ram jet burning magnesium slurry fuel and having a conical shock inlet designed for a Mach number of 4.1
- Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree sweptback wing
- Flutter at very high speeds
- Flutter investigation at low speed of a 40 degree sweptback wing with pylon-mounted stores, tested as a semispan-cantilever wing and as a full-span wing on a towed airplane model
- Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99, [Part] 2, Isentropic-spike all-external compression inlet
- Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration
- Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration
- Fuel characteristics pertinent to the design of aircraft fuel systems : Supplement 1 - Additional information on MIL-F-7914(AER) Grade JP-5 fuel and several fuel oils
- Generalization of boundary-layer momentum-integral equations to three-dimensional flows including those of rotating system
- Graph embedding techniques for bounding condition numbers of incomplete factor preconditioners
- Graph embeddings and Laplacian eigenvalues
- Heat transfer on an afterbody immersed in the separated wake of a hemisphere
- Heat-transfer processes in liquid-cooled engine cylinders : 1 - Correlation of single-cylinder engine temperatures under forced-convection cooling conditions
- Heat-transfer tests of aqueous ethylene glycol solutions in an electrically heated tube
- Hydrodynamic-stability tests of a model of a flying boat and of a planing surface having a small downward projection (hook) on the planing bottom near the step
- Informational diagram collection /c[editor, Yu Fukushi ; coordinator, Maya Kishida ; photographer, Kuniharu Fujimoto ; translators, Maya Kishida, Pamela Miki]
- Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region
- Internal performance characteristics of short convergent-divergent exhaust nozzles designed by the method of characteristics
- Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45° sweptback highly tapered wing in combination with basic and indented bodies
- Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles
- Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination
- Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections
- Investigation of a simple device for preventing separation due to shock and boundary-layer interaction
- Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air
- Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds
- Investigation of the NACA 4-(4)(06)-04 two-blade propeller at forward Mach numbers to 0.925
- Investigation of the NACA-4-(3)(08)-03 two-blade propeller at forward Mach numbers to 0.925
- Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord
- Investigation of the aerodynamic characteristics in pitch and sideslip of a 45° swept-wing airplane configuration with various vertical locations of the wing and horizontal tail : Static lateral and directional stability ; Mach numbers of 1.41 and 2.01
- Investigation of three types of supersonic diffuser over a range of Mach numbers from 1.75 to 2.74
- Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6
- Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
- Knock-limited performance of pure hydrocarbons blended with a base fuel in a ful-scale, aircraft-engine cylinder : 3 - Four aromatics, six ethers
- Knock-limited performance tests of 2,2,3,4-tetramethylpentane, 2,3,3,4-tetramethylpentane, 3,4,4-trimethyl-2-pentene, and 2,3,4-trimethyl-2-pentene in small-scale and full-scale cylinders
- Knocking tendency of an air-cooled aircraft-engine cylinder with one and with two spark plugs
- Langley full-scale tunnel investigation of the factors affecting the directional stability and trim characteristics of a fighter-type airplane
- Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35°, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : Transonic-bump method
- Lift and drag characteristics of a low-drag airfoil with slotted flap submitted by Curtiss-Wright Corporation
- Lift-curve slopes determined in flight on a flexible swept-wing jet bomber
- Low-speed static stability characteristics of a cambered-delta-wing model
- Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing
- Measurement of the longitudinal moment of inertia of a flexible airplane
- Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds
- Nitrided-steel piston rings for engines of high specific power
- Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05
- Operating temperatures of a sodium-cooled exhaust valve as measured by a thermocouple
- Performance characteristics of a Junkers Jumo 211F engine supercharger with a DVL fully shrouded impeller and scroll diffuser
- Performance effect of fully shrouding a centrifugal supercharger impeller
- Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory
- Performance of basic XJ79-GE-1 turbojet engine and its components
- Portolan atlas,
- Power-on longitudinal-stability and control tests of the 1/8-scale model of the Brewster F2A airplane equipped with full-span slotted flaps and a new horizontal tail
- Power-on wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane with full-span slotted flaps
- Preliminary attempts at isothermal compression of a supersonic air stream
- Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet
- Preliminary investigation of the compressive strength and creep lifetime of 2024-T3 (formerly 24S-T3) aluminum-alloy plates at elevated temperatures
- Preliminary investigation of the compressive strength and creep lifetime of 2024-T3 (formerly 24S-T3) aluminum-alloy plates at elevated temperatures
- Preliminary investigation of the failure of pressurized stiffened cylinders
- Preliminary studies of rolling-contact fatigue life of high-temperature bearing materials
- Rapid graphs with Tableau 8 : the original guide for the accidental analyst
- Real-time application of advanced three-dimensional graphic techniques for research aircraft simulation
- Recommended test procedure for aircraft engine turbosupercharger power plants
- Relation of preignition and knock to allowable engine temperatures
- Reliability models for dataflow computer systems
- Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range
- Shear-lag tests of a box beam with a highly cambered cover in tension
- Small-orifice tubes for minimizing dilution in exhaust-gas samples
- Some effects of external wing tip stores on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick tapered, unswept wing
- Some observations on loss of static strength due to fatigue cracks
- Some recent research on the handling qualities of airplanes
- Span loadings due to wing twist at transonic and supersonic speeds
- Spinning and related problems at high angles of attack for high-speed airplanes
- Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4
- Static-thrust tests of six rotor-blade designs on a helicopter in the Langley full-scale tunnel
- Statistical survey of icing data measured on scheduled airline flights over the United States and Canada from November 1951 to June 1952
- Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds
- Strain measurements and strength tests of 25-inch diagonal-tension beams with single uprights
- Supersonic flutter of a 60° delta wing encountered during the flight test of a rocket-propelled model
- Survey of hydrogen combustion properties
- Sway for dummies course, Adding charts to a Sway
- Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds
- Tensile properties of some sheet materials under rapid-heating conditions
- Tensile properties of some sheet materials under rapid-heating conditions
- Test data on the shear strength of joints assembled with round-head and brazier-head rivets
- Test of NACA 66,2-116, a : 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane
- Tests of 10 inch 24S-T aluminum-alloy shear panels with 1-1/2 inch holes : 2 - Panels having holes with notched edges
- Tests of a small-scale NACA submerged inlet at transonic Mach numbers
- Tests of four models representing intermediate sections of the XB-33 airplane including sections with slotted flap and ailerons
- The Influence of very heavy fuselage mass loadings and long nose lengths upon oscillations in the spin
- The NACA balanced-diaphragm dynamometer-torque indicator
- The SMARTSat redesign study
- The beauty of diagrams, Episode 1, Vitruvian man & DNA
- The beauty of diagrams, Episode 2, Newton's prism & Florence Nightingale
- The beauty of diagrams, Episode 3, Copernicus & Pioneer plaque
- The effect of increase in combustion-air inlet temperature from 80 to 130 degrees F on the sea-level performance of a 22-inch-diameter pulse-jet engine
- The effect of inlet temperature and pressure on the efficiency of a single-stage impulse turbine having a 13.2-inch pitch-line diameter wheel
- The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion
- The effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel
- The knock-limited performance of fuel blends containing aromatics : 4 - Data for m-diethylbenzene, 1-ethyl-4-methylbenzene and sec-butylbenzene together with a summarization of data for 12 aromatic hydrocarbons
- The knock-limited performance of fuel blends containing aromatics : 5 - n-propylbenzene, n-butylbenzene, isobutylbenzene, m-xylene, and 1-isopropyl-4-methylbenzene
- The performance of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with cast airfoil-shaped and bent sheet-metal nozzle blades
- The rolling moment due to sideslip of swept wings at subsonic and transonic speeds
- The science of analyzing : forming and proving conclusions by the use of charts, lesson 1-15
- The strength and stiffness of shear webs with and without lightening holes
- The strength and stiffness of shear webs with round lightening holes having 45 degree flanges
- Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase against maneuvering and nonmaneuvering targets
- Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas
- Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds : Subsonic leading edges and trailing edges
- Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition
- Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds
- Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches
- Transonic wind-tunnel investigation of aerodynamic-loading characteristics of a 2-percent-thick trapezoidal wing in combination with basic and indented bodies
- Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6
- Variation of peak pitching-moment coefficients for six airfoils as affected by compressibility
- Vertical and drag ground-reaction forces developed in landing impacts of a large airplane
- Visual study of free convection in a narrow vertical enclosure
- Wind tunnel investigation of a plain aileron with various trailing-edge modifications on a tapered wing : 1- Aileron with fixed inset tabs
- Wind tunnel investigation of control surface characteristics : 12 - Various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance
- Wind tunnel investigation of effect of yaw on lateral-stability characteristics : 4 - Symmetrically tapered wing with a circular fuselage having a wedge-shaped rear and a vertical tail
- Wind-tunnel investigation of a revised horizontal tail surface for the Grumman TBF-1 airplane
- Wind-tunnel investigation of ailerons on a low-drag airfoil : 1 - The effect of aileron profile
- Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack
- Wind-tunnel investigation of effects of ventral fins at two positions on lateral-stability derivatives of 45° high-wing model oscillating in yaw
- Wind-tunnel investigation of shielded horn balancees and tabs on a 0.7-scale model of XF6F vertical tail surface
- Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing-fuselage combination having a triangular wing of aspect ratio 4
- Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds
- Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modification of aileron nose and adjacent airfoil contour
- Word 2016 for dummies adding tables & objects course, Creating a chart in Word 2016
- Wordless diagrams
- [Representing spatial information in a computational model for network management] : resubmission of final report

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