DOWNLOADABLE COURSE MATERIALS (Cengiz Camci)
COURSE OBJECTIVES , OUTLINE AND DETAILS (56 Kb) 
INTRODUCTORY LECTURE on 28-AUGUST-2002 WEDNESDAY ( 4.9 Mb)
SPACE SHUTTLE MAIN ENGINE SCHEMATIC (216 Kb)
SECOND LECTURE on 30-AUGUST-2002 FRIDAY (796 Kb)
THIRD & FOURTH LECTURE on 4-SEPTEMBER-2002 WEDNESDAY (656 Kb)
HOMEWORK#1 DUE 11-WEDNESDAY-2002 12:20 (36 Kb)
HOMEWORK#1 SOLUTIONS (248 Kb)
FIFTH&SIXTH LECTURE on 9-SEPTEMBER-2002 MONDAY (624Kb)
SEVENTH LECTURE part.1 on 13-SEPTEMBER-2002 FRIDAY(680Kb)
EIGHT LECTURE on 16-SEPTEMBER-2002 MONDAY(344Kb)
HOMEWORK#2 DUE 18-SEPTEMBER-2002 WEDNESDAY (48 Kb)
HOMEWORK#2 SOLUTIONS (228 Kb)
NINTH LECTURE on 18-SEPTEMBER-2002 WEDNESDAY (635Kb)
SEVENTH LECTURE CONTINUED part.2 20-SEPTEMBER-2002 FRIDAY by: DANIEL CLEMENS (see lecture_seven.ppt)
SEVENTH LECTURE CONTINUED part.3 23-SEPTEMBER-2002 MONDAY by : DANIEL CLEMENS (see lecture_seven.ppt)
TENTH LECTURE on 25-SEPTEMBER-2002 WEDNESDAY (1300Kb)
ELEVENTH LECTURE on 27-SEPTEMBER-2002 FRIDAY (956Kb)
LECTURE 12 (524Kb)
READING MATERIAL FROM HILL&PETERSON (84Kb)
" HOMEWORK#3 DUE 24-SEPTEMBER-2002 (52 Kb)
" HOMEWORK#3 SOLUTIONS (576 Kb)
COMPUTER PROJECT # 1/Auxiliary Power Unit (Turbo-shaft Engine Analysis) DUE 9-OCTOBER-2002 WEDNESDAY (1400 Kb)
MID TERM EXAM 1 & SOLUTIONS 9-OCTOBER-2002 WEDNESDAY (1700 Kb)
13. INTRODUCTION TO TURBO-FANS Part-1 (600Kb)
14. INTRODUCTION TO TURBO-FANS Part-2 (740Kb)
15. BY-PASS /TURBO-FAN ENGINES-1 (1300Kb)
16. BY-PASS /TURBO-FAN ENGINES-2 (1390Kb)
17. BY-PASS /TURBO-FAN ENGINES-3 (1700Kb)
18. GE 90 A HIGH BY PASS RATIO TURBO-FAN FOR BOEING 777 (608Kb)
COMPUTER PROJECT # 2/TURBO-FAN DESIGN STUDY (320Kb)
GE 90 (technical paper) (1300Kb)
JET BLAST a short movie about jet power (984Kb)
19. TURBO-SHAFT/TURBO-PROP ENGINES (780Kb)
20. PROPELLER DESIGN 1 (1060Kb)
21. PROPELLER DESIGN 2 (688Kb)
advanced prop fan/counter rotating propeller examples (672Kb)
22. PROPELLER_DESIGN 3 (752Kb)
23. UDF (UNDUCTED FAN) ENGINE CONCEPT (1020Kb)
COMPUTER PROJECT # 3/PROPELLER DESIGN ANALYSIS (508Kb) DUE 11-NOVEMBER-2002
================================================
FINAL EXAM WILL COVER ALL OF THE TOPICS AFTER LECTURE 23
(LECTURE 23 IS NOT INCLUDED)
24. RAMJET ENGINE AS A SUPERSONIC PROPULSION SYSTEM-IDEAL CYCLE (2611Kb)
25. IDEAL RAMJET ANALYSIS (4514Kb)
26. ACTUAL RAMJET ANALYSIS (2381Kb)
27. TURBO-RAM-JET ENGINES J-58 P&W(2611Kb) 8-November-2002
28. INTRODUCTION TO SCRAMJETS (1211Kb)
29. SCRAMJET DESIGN&ANALYSIS(1499Kb)
30.a RECENT SCRAMJET/SSTO EFFORTS (1864Kb) 4-NOVEMBER-2002
30 .b NASA HYPER-X X43 PROJECT (2131Kb) 6-NOVEMBER-2002
31.a PULSATING RAMJET ENGINE ARGUS FOR V1 (ARGUS ) PART-1 (6912Kb) 8-November-2002
31.b PULSATING RAMJET ENGINE ARGUS FOR V1 PART-2 (3019Kb) 8-November-2002
ORIGINAL AAF Pulsating Ramjet Report (1082Kb) 8-NOVEMBER-2002
32. SUPERSONIC INTAKES part-A (1425Kb)
33. SUPERSONIC INTAKES part-B (1425Kb)
34. INTAKE AND NOZZLE SYSTEMS FOR THE SUPERSONIC MACH 2 TRANSPORT PLANE CONCORDE (380Kb)
supersonic intake analysis_EXAMPLES (6758Kb)
35. ROTARY ENGINES (Wankel engine) (1651Kb)
PRATT & WHITNEY TRIP 15-NOVEMBER-2002
HOMEWORK#6 DUE 26-NOVEMBER-2002 (48 Kb)
36. LABORATORY SESSION "Small Turbo-jet Engines", 22-November-2002
37. A TURBOJET ENGINE FOR SUPERSONIC PASSENGER AIRCRAFT/OLYMPUS (engine/intake/exhaust nozle) (522Kb)
38. PSU AXIAL FLOW TURBINE RESEARCH FACILITY (3652Kb)
39. AXIAL TURBINES PART-1 (1748Kb)
40. AXIAL TURBINES PART-2 (1595Kb)
41. AXIAL FLOW COMPRESSORS (1271Kb)
42. CENTRIFUGAL COMPRESSORS PART-1 (748Kb)
43. CENTRIFUGAL COMPRESSORS PART-2 (681Kb)
44. SOLID PROPELLANT ROCKETS
45. NUCLEAR ROCKETS
EXAMPLE PROBLEMS (SOLVED) (352Kb)
FINAL EXAM PROBLEMS (MSWord format) (will be available at 10:30 am 12/14/2002)
FINAL EXAM PROBLEMS (pdf) (will be available at 10:30 am 12/14/2002)
DEPARTMENT OF AEROSPACE ENGINEERING
BACK TO HOME PAGE
PROPULSION SEMINAR FALL 2002
d
Small_Engines
GE_90
SOPHIA_850
WANKEL_SCRC
woodpecker
450_1_movie
450_2_movie
450_2_movie
UCAV_MAY
UCAV_NOV
USEFUL FILES FOR SMALL PROPULSION SYSTEMS
USED IN UN-MANNED AIRCRAFT
UAV PROPULSION SYSTEMS
TRANSATLANTIC FLIGHT WITH UAV
FOUR STROKE ENGINES
ANIMATION OF FOUR CYCLE ENGINES
ANIMATION OF TWO STROKE ENGINES
ANIMATION OF A WANKEL (ROTARY) ENGINE
COURSE OBJECTIVES , OUTLINE AND DETAILS (56 Kb)
INTRODUCTORY LECTURE on 28-AUGUST-2002 WEDNESDAY ( 4.9 Mb)
SPACE SHUTTLE MAIN ENGINE SCHEMATIC (216 Kb)
SECOND LECTURE on 30-AUGUST-2002 FRIDAY (796 Kb)
THIRD & FOURTH LECTURE on 4-SEPTEMBER-2002 WEDNESDAY (656 Kb)
HOMEWORK#1 DUE 11-WEDNESDAY-2002 12:20 (36 Kb)
HOMEWORK#1 SOLUTIONS (248 Kb)
FIFTH&SIXTH LECTURE on 9-SEPTEMBER-2002 MONDAY (624Kb)
SEVENTH LECTURE part.1 on 13-SEPTEMBER-2002 FRIDAY(680Kb)
EIGHT LECTURE on 16-SEPTEMBER-2002 MONDAY(344Kb)
HOMEWORK#2 DUE 18-SEPTEMBER-2002 WEDNESDAY (48 Kb)
HOMEWORK#2 SOLUTIONS (228 Kb)
NINTH LECTURE on 18-SEPTEMBER-2002 WEDNESDAY (635Kb)
SEVENTH LECTURE CONTINUED part.2 20-SEPTEMBER-2002 FRIDAY by: DANIEL CLEMENS (see lecture_seven.ppt)
SEVENTH LECTURE CONTINUED part.3 23-SEPTEMBER-2002 MONDAY by : DANIEL CLEMENS (see lecture_seven.ppt)
TENTH LECTURE on 25-SEPTEMBER-2002 WEDNESDAY (1300Kb)
ELEVENTH LECTURE on 27-SEPTEMBER-2002 FRIDAY (956Kb)
LECTURE 12 (524Kb)
READING MATERIAL FROM HILL&PETERSON (84Kb)
" HOMEWORK#3 DUE 24-SEPTEMBER-2002 (52 Kb)
" HOMEWORK#3 SOLUTIONS (576 Kb)
COMPUTER PROJECT # 1/Auxiliary Power Unit (Turbo-shaft Engine Analysis) DUE 9-OCTOBER-2002 WEDNESDAY (1400 Kb)
MID TERM EXAM 1 & SOLUTIONS 9-OCTOBER-2002 WEDNESDAY (1700 Kb)
13. INTRODUCTION TO TURBO-FANS Part-1 (600Kb)
14. INTRODUCTION TO TURBO-FANS Part-2 (740Kb)
15. BY-PASS /TURBO-FAN ENGINES-1 (1300Kb)
16. BY-PASS /TURBO-FAN ENGINES-2 (1390Kb)
17. BY-PASS /TURBO-FAN ENGINES-3 (1700Kb)
18. GE 90 A HIGH BY PASS RATIO TURBO-FAN FOR BOEING 777 (608Kb)
COMPUTER PROJECT # 2/TURBO-FAN DESIGN STUDY (320Kb)
GE 90 (technical paper) (1300Kb)
JET BLAST a short movie about jet power (984Kb)
19. TURBO-SHAFT/TURBO-PROP ENGINES (780Kb)
20. PROPELLER DESIGN 1 (1060Kb)
21. PROPELLER DESIGN 2 (688Kb)
advanced prop fan/counter rotating propeller examples (672Kb)
22. PROPELLER_DESIGN 3 (752Kb)
23. UDF (UNDUCTED FAN) ENGINE CONCEPT (1020Kb)
COMPUTER PROJECT # 3/PROPELLER DESIGN ANALYSIS (508Kb) DUE 11-NOVEMBER-2002
================================================
FINAL EXAM WILL COVER ALL OF THE TOPICS AFTER LECTURE 23
(LECTURE 23 IS NOT INCLUDED)
24. RAMJET ENGINE AS A SUPERSONIC PROPULSION SYSTEM-IDEAL CYCLE (2611Kb)
25. IDEAL RAMJET ANALYSIS (4514Kb)
26. ACTUAL RAMJET ANALYSIS (2381Kb)
27. TURBO-RAM-JET ENGINES J-58 P&W(2611Kb) 8-November-2002
28. INTRODUCTION TO SCRAMJETS (1211Kb)
29. SCRAMJET DESIGN&ANALYSIS(1499Kb)
30.a RECENT SCRAMJET/SSTO EFFORTS (1864Kb) 4-NOVEMBER-2002
30 .b NASA HYPER-X X43 PROJECT (2131Kb) 6-NOVEMBER-2002
31.a PULSATING RAMJET ENGINE ARGUS FOR V1 (ARGUS ) PART-1 (6912Kb) 8-November-2002
31.b PULSATING RAMJET ENGINE ARGUS FOR V1 PART-2 (3019Kb) 8-November-2002
ORIGINAL AAF Pulsating Ramjet Report (1082Kb) 8-NOVEMBER-2002
32. SUPERSONIC INTAKES part-A (1425Kb)
33. SUPERSONIC INTAKES part-B (1425Kb)
34. INTAKE AND NOZZLE SYSTEMS FOR THE SUPERSONIC MACH 2 TRANSPORT PLANE CONCORDE (380Kb)
supersonic intake analysis_EXAMPLES (6758Kb)
35. ROTARY ENGINES (Wankel engine) (1651Kb)
PRATT & WHITNEY TRIP 15-NOVEMBER-2002
HOMEWORK#6 DUE 26-NOVEMBER-2002 (48 Kb)
36. LABORATORY SESSION "Small Turbo-jet Engines", 22-November-2002
37. A TURBOJET ENGINE FOR SUPERSONIC PASSENGER AIRCRAFT/OLYMPUS (engine/intake/exhaust nozle) (522Kb)
38. PSU AXIAL FLOW TURBINE RESEARCH FACILITY (3652Kb)
39. AXIAL TURBINES PART-1 (1748Kb)
40. AXIAL TURBINES PART-2 (1595Kb)
41. AXIAL FLOW COMPRESSORS (1271Kb)
42. CENTRIFUGAL COMPRESSORS PART-1 (748Kb)
43. CENTRIFUGAL COMPRESSORS PART-2 (681Kb)
44. SOLID PROPELLANT ROCKETS
45. NUCLEAR ROCKETS
EXAMPLE PROBLEMS (SOLVED) (352Kb)
FINAL EXAM PROBLEMS (MSWord format) (will be available at 10:30 am 12/14/2002)
FINAL EXAM PROBLEMS (pdf) (will be available at 10:30 am 12/14/2002)
DEPARTMENT OF AEROSPACE ENGINEERING
BACK TO HOME PAGE PROPULSION SEMINAR FALL 2002
d
Small_Engines
GE_90
SOPHIA_850
WANKEL_SCRC
woodpecker
450_1_movie
450_2_movie
450_2_movie
UCAV_MAY
UCAV_NOV
USEFUL FILES FOR SMALL PROPULSION SYSTEMS USED IN UN-MANNED AIRCRAFT
UAV PROPULSION SYSTEMS
TRANSATLANTIC FLIGHT WITH UAV
FOUR STROKE ENGINES
ANIMATION OF FOUR CYCLE ENGINES
ANIMATION OF TWO STROKE ENGINES
ANIMATION OF A WANKEL (ROTARY) ENGINE