Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
Thermal characteristics of rocket propellants
Download
093298.pdf
Date
2000
Author
Fazlıoğlu, Hatice
Metadata
Show full item record
Item Usage Stats
54
views
0
downloads
Cite This
URI
https://hdl.handle.net/11511/2649
Collections
Graduate School of Natural and Applied Sciences, Thesis
Suggestions
OpenMETU
Core
Thermal and mechanical properties of rocket motor liners
Benli, Salih; Yılmazer, Ülkü; Özkar, Saim; Department of Chemical Engineering (1997)
Rocket motor liners are usually chosen from filled elastomers. The primary function of the liner layer is to bind the propellant grain to the motor case. A rocket motor liner also serves as a thermal insulator and burning inhibitor during the operation of the rocket motor. The primary objective of this study was to make thermal and mechanical characterization of polyurethane based rocket motor liners, and develop new liner compositions with optimum thermal, mechanical and processing properties. In the first...
Thermal characteristics and kinetics of crude oils and SARA fractions
Kök, Mustafa Verşan (Elsevier BV, 2013-10-10)
In this study, two Turkish crude oils from southeastern part of Turkey and their saturate, aromatic and resin fractions were analyzed by thermogravimetric analysis (TGA). The experiments were performed at three different heating rates (5, 10, 15 degrees C/min) under air atmosphere. Two different reaction regions were observed from thermogravimetry (TG), differential thermogravimetry (DTG) curves due to the oxidative degradation of crude oil components. From TGA curves, it was detected that the heavier fract...
Thermal and mechanical properties of Pt-Rh alloys
Dereli, G; Cagin, T; Uludogan, M; Tomak, Mehmet (1997-04-01)
We utilize the many-body potentials developed by Sutton and Chen within the context of the tight-binding approach to study the bulk properties of metals and metal alloys in molecular dynamics (MD) simulations. In the simulations of Pt-Rh alloys we used the MD algorithms based on an extended Hamiltonian formalism from the works of Andersen, Parrinello and Rahman, Nose, Hoover, and Cagin. The simulator program that we use generates information about various physical properties during the run time, along with ...
Thermal properties of polyethylene and polypropylene blends.
Atalay, Arzu; Tinçer, Teoman; Department of Chemistry (1996)
Thermal management of solid oxide fuel cells by flow arrangement
Şen, Fırat; Tarı, İlker; Department of Mechanical Engineering (2012)
Solid oxide fuel cell (SOFC) is a device that converts the chemical energy of the fuel into the electricity by the chemical reactions at high temperatures (600-1000oC). Heat is also produced besides the electricity as a result of the electrochemical reactions. Heat produced in the electrochemical reactions causes the thermal stresses, which is one of the most important problems of the SOFC systems. Another important problem of SOFCs is the low fuel utilization ratio. In this study, the effect of the flow ar...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
H. Fazlıoğlu, “Thermal characteristics of rocket propellants,” Middle East Technical University, 2000.