MARC details
| 000 -LEADER |
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| fixed length control field |
02472nam a2200253 a 4500 |
| 001 - CONTROL NUMBER |
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| control field |
vtls000069523 |
| 003 - CONTROL NUMBER IDENTIFIER |
|---|
| control field |
KUKTEM |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20251114204536.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
130514t2012 my da f m 000 0 eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
THE0007344(Local) |
| 039 #9 - LEVEL OF BIBLIOGRAPHIC CONTROL AND CODING DETAIL [OBSOLETE] |
|---|
| Level of rules in bibliographic description |
201905151012 |
| Level of effort used to assign nonsubject heading access points |
fawwaz |
| -- |
201305141153 |
| -- |
Fida |
| 040 ## - CATALOGING SOURCE |
|---|
| Original cataloging agency |
UMP |
| 090 ## - LOCALLY ASSIGNED LC-TYPE CALL NUMBER (OCLC); LOCAL CALL NUMBER (RLIN) |
|---|
| Classification number (OCLC) (R) ; Classification number, CALL (RLIN) (NR) |
TL278 .C44 2012 rs Bc. |
| 100 0# - MAIN ENTRY--PERSONAL NAME |
|---|
| Personal name |
Che Muhammad Ridhwan Che Hashim |
| 245 10 - TITLE STATEMENT |
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| Title |
Design, detail analysis and performance testing of uav propulsion system / |
| Statement of responsibility, etc. |
Che Muhammad Ridhwan Che Hashim |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. |
|---|
| Place of publication, distribution, etc. |
Kuantan, Pahang : |
| Name of publisher, distributor, etc. |
UMP, |
| Date of publication, distribution, etc. |
2012 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
xiv, 62 p. : |
| Other physical details |
ill. (some col.) ; |
| Dimensions |
30 cm. + |
| Accompanying material |
1 CD-ROM |
| 502 ## - DISSERTATION NOTE |
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| Dissertation note |
Project paper (Bachelor of Mechanical Engineering with Automotive Engineering) -- Universiti Malaysia Pahang - 2012 |
| 504 ## - BIBLIOGRAPHY, ETC. NOTE |
|---|
| Bibliography, etc. note |
Bibliography : p. 51-52 |
| 520 3# - SUMMARY, ETC. |
|---|
| Summary, etc. |
This project report is being conduct because the use of an Unmanned Aerial Vehicle (UAV) is getting popular among people either to have fun or study but the choices of powerplant are not fully deployed (in term of operational and performance sizing) and thus limiting the selection. The objective of this project is to propose a design, detail analysis and performance testing of an Unmanned Aerial Vehicle (UAV) propulsion system. In this study, the test bed model was designed to test the nitro engine Radio Control (RC) which is model of 46-LA OS Engine Series of aircraft performance which are four performance parameters that was studied such as thrust, available power and shaft brake power, propulsive efficiency and brake specific fuel consumption thus the performance parameters value can be calculated by measure the unknown value of parameters regarding to the equation involves within the range 2000 to 16000 RPM of engine speed by setting the test bed design with suitable apparatus. From this experiment, the result shows that the fabricated test bed can be use to study the engine performance and performance parameters are directly proportional to the engine speed which is mean the faster the speed of engine effected the increasing of performance parameters. As a conclusion, even without testing the engine to the real body of aircraft, all the engine performance parameter can be calculated from this experiment, and it will reduce the time and cost. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Embedded computer systems |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Drone aircraft |
| General subdivision |
Automatic control |