bluuebunny/crossref_metadata_2025_split huggingface dataset:
PENGARUH PRODUK, HARGA, TEMPAT, PROMOSI TERHADAP KEPUTUSAN PEMBELIAN PIZZA HUT DELIVERY GRESIK
Authors: Jeni Adel Trudis Nurya 
Published: May 2019

Abstract
The purpose of this study was to determine whether the product, price, place and sales promotion variables partially had an influence on the purchasing decision at Pizza Hut Delivery Gresik. The type of data used is primary data. Primary data was obtained through direct interviews with the Pizza Hut Delivery Gresik Manager. The data analysis technique used is multiple linear regression whose purpose is to calculate the magnitude of the regression coefficient which will show the magnitude of the influence of the independent variables consisting of product variables, prices, places, and sales promotions on purchasing decisions. Based on the results of this study indicate that product variables, prices, places, and sales promotions partially influence the purchase decision variables.
İŞGÖRENLERİN SOSYAL VE BEŞERİ SERMAYE DÜZEYLERİ İLE İŞTEN AYRILMA NİYETLERİ ARASINDAKİ İLİŞKİNİN TESPİTİNE YÖNELİK BİR ALAN ARAŞTIRMASI
Authors: ABA ŞENBAYRAM Emel 
Published: May 2019

Tarafların ekonomik alandaki başarısı sadece sahip olduğu
finansal varlık, yetenekler veya sosyal ağlara bağlı değil aynı zamanda
çalışanlarının da beşeri ve sosyal yeteneğine bağlıdır. Sosyal ve beşeri
anlamda güçlü olan işgörenler bulundukları yerlere maddi, manevi katkılar
sağlarken yokluklarıyla söz konusu yerlerde bir takım kayıplara sebep
olabilmektedirler.

Çalışmada, işgörenlerin
sosyal ve beşeri sermaye birikimleri ile işten ayrılma niyetleri ile arasındaki
ilişkinin tespiti amaçlanmıştır. Bu amaçla, GAP Bölgesini temsilen Şanlıurfa,
Gaziantep ve Diyarbakır’daki banka yetkililer üzerinde bir araştırma yapılmıştır.
Araştırma sonucunda işgörenlerin sosyal ve beşeri sermaye
birikimlerinin iş tatmin düzeyleri üzerinde etkili olduğu ve işten ayrılma
niyeti ile ilişkili olduğu tespit edilmiştir.
COMPARATIVE ANALYSIS OF THE EFFICIENCY OF MODERN METHODS FOR DETERMINATION OF YOUNG DUCKS SEX
Authors: Bondarenko Yu. V. , Shkurko М. I. 
Published: May 2019

Experimental researches were carried out during the years 2012–2017 at the farm "Povit-Agro", Bila Tserkva region, Kyiv Oblast, as well as at other farms. 1390 Ukrainian mulards were bred during these 2 years. Throughout our researches the French mulard was presented with 2425 1-day-old hybrid ducklings. In addition, during the studies, the 1-day-old ducklings of different breeds were assessed, namely ducklings of a domestic duck – 7579 heads, ducklings of a musk duck – 1685 heads.
A comparative analysis of the effeciency of modern methods for determining the sex of young ducks of two species and of interspecies hybrid is conducted. It has been found that the highest accuracy of duckling sex determination (100%) of all genotypes is provided by the universal Japanese method (ventsexing), and a specific method - colorsexing (based on genetic markers of down coloring). Sidorov's method (probing of resonator of males) allows to determine the sex of domestic (but not musk) and mullard ducklings with an accuracy of 94–98% at a sorting rate of 300 g/h. The anatomical method is absolutely accurate, but it is associated with young ducks slaughtering. Morphosexing is effective for ducklings of all studied genotypes starting from the 2-month age .
Morphosexing is effective for ducklings starting from the 2-month old of all studied genotypes. Beginning from 60 days old, the sex of ducklings of a musk duck, as well as mulards, can be determined due to the color and size of skin folds around the upper part of the beak with an accuracy of 97–99%. For the 2-month old ducklings of a domestic duck, sexual dimorphism is clearly expressed according to the other two features. Males at this age already have two twisted feathers in their tails, and females, unlike males, can quack loudly.
Failure of Aircraft Engine Crankshaft
Authors: Craft C. Howard 
Published: May 2019

Abstract
A broken aircraft crankshaft and a severely damaged main brass bearing were examined to determine whether engine failure was initiated in the bearing or in the crankshaft. The steel crankshaft failure was a classical fatigue fracture. The bearing had been subjected to extremely high temperatures, as indicated by melting in the brass components and the extreme distortion in the rollers. Microscopic examination on the crankshaft material showed it to be a good quality steel. On the other hand, the chromium plate was thick, porous, and cracked in many places, including the point of the main fatigue crack. It was concluded that the over-all failure was initiated in the crankshaft, and the failure of the bearing resulted from that failure.
Dimpling of Aluminium Sheet
Authors: Wittig Ruth , Rickel Jürgen 
Published: May 2019

Abstract
Countersunk riveted joints in aluminum sheet are widely employed in the aircraft industry. The preparation of the sheet for the riveting process consists either of countersinking where the sheet is sufficiently thick or of dimpling. Metallographic assessment of dimple defects is described in specimens made of clad aluminum sheet of alloy type AlZnMgCu1.5. Addressed are a dimple with partially missing stamped surface (bell-mouth), a cylindrical prominence because the dimpling force was too great and the stamping cylinder force too low, and a dimple with flashes at the top surfaces of the sheet as a result of play between the stamping cylinder and the anvil head (ringed dimple). Frequently, overlapping of several defects occurs, especially with steel or titanium sheet, with the result that it is difficult to identify the defects.
Use of Electron Fractography to Diagnose Cracking in an AISI 4340 Nose Landing Gear Cylinder
Authors: Scott James A. 
Published: May 2019

Abstract
Examination of a cracked nose landing gear cylinder made of AISI 4340 Cr-Mo-Ni alloy steel proved that the part started to fail on the inside diam. When the nucleus of the stress-corrosion crack was studied in detail, iron oxide was found on the fracture surface. A 6500x micrograph revealed this area also displayed an intergranular texture. One of a group of small grinding cracks on the ID of the cylinder nucleated the failure. Other evidence indicated the cracks developed when the cylinder was ground during overhaul.
Failures in Airplane Engine Crankshafts
Authors: Shah Jivan B. 
Published: May 2019

Abstract
This report covers case histories of failures in fixed-wing light aeroplane and helicopter components. A crankshaft of AISI 4340 Ni-Cr-Mo alloy steel, heat treated and nitrided all over, failed in bending fatigue. The nitrided layer was ground too rapidly causing excessive heat generation which induced grinding cracks and grinding burn. Tensional stresses resulting from grinding developed in a thin surface layer. On another crankshaft, chromium plating introduced undesirable residual tensile stresses. Such plating is an unsatisfactory finish for crankshafts of aircraft engines. Aircraft engine manufacturers and aeronautical standards require magnetic particle inspection to detect grinding cracks after reconditioning. Renitriding after any grinding is needed also, regardless of the amount of undersize as it introduces beneficial residual compressive stresses.
Stress Corrosion Cracking of 4340 Steel in Aircraft Ignition Starter Residues
Authors: Kennelley Kevin J. , Daniels Raymond D. 
Published: May 2019

Abstract
Military aircraft use a cartridge ignition system for emergency engine starts. Analysis of premature failures of steel (AISI 4340) breech chambers in which the solid propellant cartridges were burned identified corrosion as one problem with an indication that stress-corrosion cracking may have occurred. A study was made for stress-corrosion cracking susceptibility of 4340 steel in a paste made of the residues collected from used breech chambers. The constant extension rate test (CERT) technique was employed and SCC susceptibility was demonstrated. The residues, which contained both combustion products from the cartridges and corrosion products from the chamber, were analyzed using elemental analysis and x-ray diffraction techniques. Electrochemical polarization techniques were also utilized to estimate corrosion rates.
Failure Investigations of PH 13-8 Mo Aircraft Components
Authors: Roth M. , Lelièvre C. 
Published: May 2019

Abstract
The failures of two aircraft components, one from a landing gear and the other from an ejector rack mechanism, were investigated. Both were made from PH 13-8 Mo (UNS S13800) precipitation-hardening stainless steel which had been heat treated to the H1000 and H950 tempers respectively and then chromium plated. The parts were characterized metallographically and mechanically and were found to be compliant. Detailed fractographic examination revealed that the first stage of both failures was similar: subsurface initiation of numerous cracks with a wide range of orientations and cleavage like features. The cracking was followed by fatigue in one case and catastrophic failure in the other. Hydrogen embrittlement was identified as the most likely mechanism of failure.
Investigation on a Damaged Propeller Blade
Authors: Pussegoda L.N. , Malik L. 
Published: May 2019

Abstract
The paper describes the findings from a damaged propeller blade made from Mn-Ni-Al-bronze, commercially known as Superston 70 (ABS Type 5). The blade had broken at the 0.65 pitch radius location, and the fracture occurred in a brittle mode. The findings reported here point to two potential contributors to the propeller blade failure, viz., the presence of casting flaws at the low pressure side of the propeller blade and service stresses at this surface that reached approximately 400 MPa. This stress value exceeded the yield strength at the corresponding location of the unbroken blade by approximately 40%.
Corrosion-Induced Failures in Aircraft Components
Authors: Shah Jivan B. 
Published: May 2019

Abstract
A steel eyebolt which attached a rear lift strut to the right wing of a helicopter failed by fatigue. As a contributing factor, thread cutting produced sharp notches at thread roots, reducing fatigue life. Also, design fatigue life may have been exceeded as the part was in use about 10,000 h. Cumulative damage resulting from a previous accident could have occurred too. Because of this accident, inspectors were instructed to examine threaded zones of eyebolts by magnetic particle inspection after every 100 h in service. A maraging steel drive shaft of a helicopter also failed because of corrosion (pits), and continuous abnormal misalignment as well. Corrosion probably developed from moisture and water droplets on shaft diaphragm profiles. Improved diaphragm pack seals and coatings made by an electron-coat process (such as a Sermetal finish) are now used in new shafts.
Failure of a Stainless Steel Bomb Fin Retaining Band
Authors: Pepi M. 
Published: May 2019

Abstract
A bomb retaining ring fabricated from type 302 stainless steel unwrapped during a practice flight, causing the bomb fins to deploy. The retaining ring was able to unwrap itself because it was thinner and softer than required. Hardness testing, metallography, and tensile testing confirmed that the component was in the annealed condition and not in the required work-hardened 1/4-hard condition.
Failure of a Steel Bomb Suspension Lug
Authors: Pepi M. 
Published: May 2019

Abstract
Suspension lugs fabricated from AISI 4340 steel used to facilitate loading of bombs onto the underside of military aircraft could not sustain required loads during routine proof load testing. Three failed lugs underwent visual examination, chemical analysis, metallography, hardness testing, scanning electron microscopy, and energy-dispersive x-ray spectroscopy. It was determined that the failures were due to forging defects. Both forging laps and seams acted as stress concentrators when the lugs were loaded during proof testing.
Failure Analysis of Welded Low-Carbon Steel Storage Tank
Authors: Suess Steven J. 
Published: May 2019

Abstract
Welded steel storage vessels used to hold mildly alkaline solution were produced in exactly the same manner from deep-drawn aluminum-killed SAE 1006 low-carbon steel sheet. After the cylindrical shell was drawn, a top low-carbon steel closure was welded to the inside diameter. The containers were then filled with the slightly alkaline solution, pressurized, and allowed to stand under ambient conditions. A small number, less than 1%, were returned because they began to leak in service. Inspection revealed general corrosion and pitting on the inner surfaces. However, other tanks that experienced the same service conditions developed no corrosion. Corrosion was linked to forming defects that provided sites for localized corrosion, and to lack of steam drying after cleaning, which increased susceptibility to general corrosion.
Corrosion Fatigue, Stress-Corrosion Cracking and Hydrogen-Sulphide Attack of AISI 304 Stainless Steel
Authors: Kenny Philip J. 
Published: May 2019

Abstract
Three separate corrosion mechanisms were involved in the failure of an AISI type 304 stainless steel pipe elbow. The major cracks, including the one that penetrated the wall, tend to be wide-mouthed, tapering to a blunt tip, with corrosion products filling much of the crack space. This was characteristic of corrosion fatigue. The second type of cracking originated at some of the major cracks. These cracks were branched and transgranular, which is characteristic of stress-corrosion caused by chlorides. The third crack mode, an intergranular network, was most probably the result of hydrogen sulphide attack. The 13-year service life of the elbow made it difficult, if not impossible, to determine the order of the corrosion mechanisms or the length of time it took to reach the present state of degradation after the initiation of corrosion. Based on the long service life the present material has given, it was recommended that it be used again.
Metallographic Studies of a Reformer Tube Failure Due to Thermal Fatigue
Authors: da Silveira Tito Luiz , Moreira Francisco Solano , Chavez Miriam Conçeicão Garcia , Le May Iain 
Published: May 2019

Abstract
The failure of a reformer tube furnace manifold has been examined using metallography. It has been shown that the cause of failure was thermal fatigue; the damage was characterized by the presence of voids produced by creep mechanisms operating during the high temperature cycle under high local stress. The study indicates that standard metallographic procedures can be used to identify failure modes in high temperature petrochemical plants.
Damages in Gears in the Transmission System of Heavy Duty Tracked Vehicles
Authors: Chatterjee P. K. 
Published: May 2019

Abstract
Failure occurred in the teeth of a case-hardening Ni-Cr-Mo alloy steel spur gear in the transmission system of heavy duty tracked vehicles. The defects were in the nature of seizure on the involute profile. Scrutiny of the transmission system showed there might be choking in the lubricating oil line. Such would cause seizure of the gears and damage. The incidence of such defects stopped after corrective measures were taken.
Mobile Harbor Crane Wheel Hub Fatigue Failure
Authors: Shirokoff J. 
Published: May 2019

Abstract
Failure analysis of a mobile harbor crane wheel hub that included SEM and EDS analyses demonstrated that the mechanism of failure was fatigue. The wheel hub was a ductile cast iron component that had been subjected to cyclic loading during a ten-year service period. The fracture surface of the fatigue failure also contained corrosion deposit, suggesting that cracking occurred over a period of time sufficient to allow corrosion of the cracked surfaces. Replacement and alignment of the failed wheel hub was recommended along with inspection of the nonfailed wheel hubs that remained on the crane.
Failures of Jib Tie-Bar Components of Tower Cranes Manufactured from Rimming Steel
Authors: Hutchings F. R. , Hanley G. 
Published: May 2019

Abstract
A new crane failed during the overload test following erection. A test load of 5 tons at the end of the jib (rated capacity 4 tons) was in the process of being slewed at the time of this failure. Inspection revealed that the collapse had resulted from the opening out of one eye of the rimming steel tie-bar of the main jib at the lower splice. This permitted the pin to pass through and allowed the jib to fall. Examination subsequently revealed that brittle fracture of two of the corner angles of the tower head assembly had also occurred. Had the tie-bar material been of satisfactory quality and/or, if the end that failed had been flamecut instead of sheared, then the damage resulting from the excessive overload would have been limited to yielding of the material in the region of the pin-joint. Such yielding on an overload test further indicated that the scantlings of the pin-joints were inadequate. Two other crane failures showed that failure resulted from the use of rimming steel, and embrittlement of the material was evident.
Prematurely Broken Valve Spring
Authors: Naumann Friedrich Karl , Spies Ferdinand 
Published: May 2019

Abstract
A valve spring made of 4.1 mm diam wire, designed to withstand 10,000,000 stress cycles, fractured after only 2,000,000 cycles. The surface displayed impressions which indicated it had been treated by shot blasting. The spring has broken in two places. Fracture 1 was a torsional fatigue fracture which has started from a lobe-like surface defect and not, as is usual, from a point on the most highly stressed inner surface. Fracture 2, on the other hand, was a bending fatigue fracture with a starting point on both the inner and the outer surface of the spiral. The objective of the shot blasting, to put the surface into a state of even compressive internal stress, which must first be overcome during subsequent bending and torsional loading before the boundary zone comes under tensile stress, was therefore not realized in this case. On the contrary, the shot blasting led to a state of internal stress which favored fracture of the spring.
Cast Steel Pinion Gear Shafts with Insufficient Elongation
Authors: Naumann Friedrich Karl , Spies Ferdinand 
Published: May 2019

Abstract
The specified elongation of 10% could not be achieved in several hollow pinion gear shafts made of cast Cr-Mo steel GS 35 Cr-Mo 5 3 that were heat treated to a strength of 90 kp/sq mm. The steel was melted in a basic 3 ton arc furnace and deoxidized in the furnace and in the pan with a total of 7 kg aluminum. Fracture of a tensile specimen occurred with low elongation and, apparently, also with low reduction of area. In some places it was coarse grained conchoidal. It was found that the exceptionally low elongation of the cast specimens was due to excessive deoxidation by aluminum.
Fatigue Fracture and Weld
Authors: Naumann Friedrich Karl , Spies Ferdinand 
Published: May 2019

Abstract
Thermal and transformation stresses, resulting from welding, adding up with operational stresses can result in failure. Examples involving the crankshaft of a shaft-drive to produce artificial waves in a swimming pool, the joint bar of a dredger cast out of a running non-alloyed steel with 39 kg/sq mm tensile strength, which had been strengthened by welding plate strips on both sides had fractured in service; an axle tube out of 40 Mn 4 after DIN 17 200 from a paper fabrication machine, which had three short longitudinal slits distributed uniformly over its surface; welding to repair worn out bearing or fits, and a broken rear axle tube of a bus are described.
Fractured Three-Cylinder Crankshaft
Authors: Naumann Friedrich Karl , Spies Ferdinand 
Published: May 2019

Abstract
The fracture cause had to be determined in a three-cylinder crankshaft made of chrome steel 34Cr4 (Material No. 1.7033) according to DIN 17200. The fracture occurred after only 150 h of operation. The fracture was of the bend fatigue type which originated in the fillet of the main bearing and ran across the jaw almost to the opposite fillet of the adjoining connecting rod bearing. The fillet was well rounded and smoothly machined. Thus, no reason for the fracture of the crankshaft could be found externally. No material defects were discernible in the origin or anywhere else. No cause for the crank fracture could be established from material testing. Probably the load was too high for the strength of the crank. Tensile strength could have been increased for the same material by tempering at lower temperature. Additionally, the resistance against high bend fatigue stresses or torsion fatigue stresses could have been increased substantially by including the fillet in the case hardening process.
Fatigue Failures, With Special Reference to Fracture Characteristics
Authors: Cottell G. A. 
Published: May 2019

Abstract
Fundamentals of fatigue failure are outlined. Addressed are fatigue crack characteristics, basic crack types, unidirectional bending, alternate bending, rotary bending, torsion, direct stress, and combined stress. Stress cycle, endurance limits, under and overstressing, stress concentration, and surface condition are discussed. Sections are devoted to fatigue crack assessment, corrosion relation to fatigue failure, and the micro-mechanisms of fatigue failure. Materials considered include steels. Photographs of service failures are used to illustrate features alluded to in the text.
Failure Analysis of a Polysulfone Flow Sensor Body — A Case Study
Authors: Jansen Jeffrey A. 
Published: May 2019

Abstract
A failure analysis was conducted on a flow-sensing device that had cracked while in service. The polysulfone sensor body cracked radially, adjacent to a molded-in steel insert. This article describes the investigative methods used to conduct the failure analysis. The techniques utilized included scanning electron microscopy, Fourier transform infrared spectroscopy, differential scanning calorimetry, thermomechanical analysis, and melt flow rate determination. It was the conclusion of the investigation that the part failed via brittle fracture, with evidence also indicating low cycle fatigue associated with cyclic temperature changes from normal service. The design of the part and the material selection were significant contributing factors because of stresses induced during molding, physical aging of the amorphous polysulfone resin, and the substantial differential in coefficients of thermal expansion between the polysulfone and the mating steel insert.
Biologically Induced Corrosion and Consequent Fracture of a Pump Shaft Coupling
Authors: Jur Tim A. 
Published: May 2019

Abstract
During a routine start-up exercise of a standby service water pump, a threaded coupling that joined sections of a 41.5 ft (12.7 m) long pump shaft experienced fracture. The pump was taken out of service and examined to determine the cause of fracture. It was apparent early in the examination that the fracture involved hydrogen stress cracking. However, the nature of the corrosive attack suggested an interaction between the threaded coupling and biological organisms living in the freshwater environment of the pump shaft. The organisms had colonized on the coupling, changing the local environment and creating conditions favorable to hydrogen stress cracking. This paper describes the analysis of the fracture of the coupling and provides an example of how biologically induced corrosion can result in unexpected fracture of a relatively basic machine part.