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)






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