ME 475/675 Introduction to Combustion Lecture 39.

Slides:

Advertisements

Similar presentations

Fig. 4-1, p Fig. 4-2, p. 109 Fig. 4-3, p. 110.

Advertisements

Combustion Design Considerations

Fuel Oil Burners.

Lecture #12 Ehsan Roohi Sharif University of Technology Aerospace Engineering Department 1.

ME 475/675 Introduction to Combustion Lecture 9. Announcements Midterm 1 September 29, 2014 (two weeks from today) HW 3 Ch 2 (57), Due now HW 4 Due Monday,

ME 475/675 Introduction to Combustion Lecture 37.

1 MAE 5310: COMBUSTION FUNDAMENTALS Introduction to Laminar Diffusion Flames Mechanical and Aerospace Engineering Department Florida Institute of Technology.

AME 513 Principles of Combustion

P.464. Table 13-1, p.465 Fig. 13-1, p.466 Fig. 13-2, p.467.

Fig. 11-1, p p. 360 Fig. 11-2, p. 361 Fig. 11-3, p. 361.

Lecture 38 CSE 331 Dec 7, The last few days Today: Solutions to HW 9 (end of lecture) Wednesday: Graded HW 9 (?), Sample final, Blog post on the.

Table 6-1, p Fig. 6-1, p. 162 p. 163 Fig. 6-2, p. 164.

COMS W1004 Introduction to Computer Science June 25, 2008.

Introduction to SEG 5010 Hong Cheng 2009/10 Second Term.

Saturday May 02 PST 4 PM. Saturday May 02 PST 10:00 PM.

ME 475/675 Introduction to Combustion Lecture 4. Announcements Extra Credit example due now HW 1 Due Friday Tutorials Wednesday 1 pm PE 113 Thursday 2.

Lon-Capa 1st HW assignment due Friday, 9/5, 5 pm. It is open now.

ME 475/675 Introduction to Combustion Lecture 21.

TODAY IN GEOMETRY…  Warm up: Writing equations of a circle  Learning Target : 11.4 You will find the arc length and circumferences of circles  Independent.

ME 322: Instrumentation Lecture 12

Business-Society Relations in Retail Value Chain (23E54000, 6cr) & Term paper presentations Mika Skippari Aalto University School of.

Chem. 31 – 2/2 Lecture. Announcements Due Wednesday –Turn in corrected diagnostic quiz –HW Set 1.1 – just additional problem Quiz on Wednesday (covering.

Introduction of jet engine

ME 475/675 Introduction to Combustion Lecture 34.

January 26, 2015 What are we doing today? 6.1 – Perimeter and Area of Rectangles and Parallelograms -Lecture and Vocabulary -HW – Practice B & C Due: Tomorrow.

Welcome to Chemistry! Please sign in at any table

Geometry Monday 8/25 Please get a piece of paper to complete the warm up…

BA271 Week 9 Lecture Three topics: o Upcoming schedule o Query Quiz review o Normalizing a database.

Wednesday, March 18 Much Ado about Nothing. Today Last Quiz: Do it with a partner but it’s CLOSED BOOK! Last Quiz: Do it with a partner but it’s CLOSED.

Understanding SSIS Control Flows Bret Stateham Training Manager Vortex Learning Solutions blogs.netconnex.com.

BR Quiz – Wolverine Wednesday. Transformations, Day 2 10/8/2014.

Today – Monday, May 20, 2013  EOC Practice Test # - First half  Learning Target : Review Ch. 10 concepts by practicing problems on a practice test 

February 9, 2015 What are we doing today? Correct 6.6 – Pg. 310 # all 6.7 – Volume of Pyramids and Cones -Lecture and Vocabulary (Pg. 312) -HW –

Lecture 5 Announcements. HW2 – Regrading Thinking like a programmer –Part b: (5 points) Test for input in the range it is specified (otherwise what is.

February 2, 2015 What are we doing today? 6.1 and 6.2 Review Due: Tomorrow Target To find the perimeter and area of rectangles and parallelograms. Question.

Extinction Limits of Catalytic Combustion in Microchannels Kaoru Maruta, Koichi Takeda Akita Prefectural University, Honjyo, Akita, Japan Jeongmin Ahn,

1 MAE 5310: COMBUSTION FUNDAMENTALS Introduction to Laminar Diffusion Flames: Non-Reacting Constant Density Laminar Jets Mechanical and Aerospace Engineering.

Analysis of Turbo Combustor P M V Subbarao Professor Mechanical Engineering Department A Device to Anchor the Flame…. The Cause of Major component of.

AP CAPSTONE SEMINAR WEEK 3.4: 12/1-5. AP Seminar Schedule 12/1  Objective: Synthesize group research and findings into a single conclusion  Essential.

ANNOUNCEMENTS. “I pledge allegiance…..” Students, please rise for the flag salute:

ME 475/675 Introduction to Combustion Lecture 40.

ME 475/675 Introduction to Combustion Lecture 38.

TODAY IN GEOMETRY…  Warm Up  Learning Goal: You will find the probability of events with and without replacement  Independent practice – 20 minutes.

Wednesday, Feb. 4, 2009PHYS , Spring 2009 Dr. Jaehoon Yu 1 PHYS 1441 – Section 002 Lecture #3 Wednesday, Feb. 4, 2009 Dr. Jaehoon Yu Dimensional.

ME 475/675 Introduction to Combustion Lecture 31 Laminar flame speed and thickness dependence on unburned temperature, pressure, fuel and dilution, Ex.

ME 475/675 Introduction to Combustion Lecture 26 Plug flow reactor, Problem X5:Constant area and pressure equations.

TODAY IN GEOMETRY…  Warm Up: Outcomes  Learning Goal: You will find the probability of events with and without replacement  Independent practice  EXIT.

Lecturer’s desk INTEGRATED LEARNING CENTER ILC 120 Screen Row A Row B Row C Row D Row E Row F Row G Row.

Wednesday, A[pril 16 th Warm-up – page 178 W-U: Explain how a tornado forms. Where do they form? Why do they form there? Get your tablet when your group.

ANNOUNCEMENTS ANNOUNCEMENTS MONDAY, NOVEMBER 2, 2015 TODAY IS A “B” DAY.

ANNOUNCEMENTS ANNOUNCEMENTS FRIDAY, NOVEMBER 13, 2015 TODAY IS AN “A” DAY.

ANNOUNCEMENTS ANNOUNCEMENTS WEDNESDAY, NOVEMBER 4, 2015 TODAY IS A “B” DAY.

University of Colorado - Intro to Aerospace Structures (ASEN 3112) - Fall 2015 Announcements (1) Last midterm exam graded, can be picked up at end of class.

ME 475/675 Introduction to Combustion Lecture 23 Example 6.1 Excel programing, Effect of equivalence ratio.

University of Wisconsin -- Engine Research Center slide 1 Flamelet Modeling for the Diffusion Combustion in OpenFOAM ME 769 Final Project Presentation.

ME 475/675 Introduction to Combustion Lecture 30 Ex. 8.2, Flame speed and thickness calculations dependence on temperature and pressure.

Energy Balance across pulverizer is very critical for satisfactory

ME 475/675 Introduction to Combustion

Problem 1 Diesel fuel (C12H26) at 25 ºC is burned in a steady flow combustion chamber with 20% excess air which also enters at 25 ºC. The products leave.

MAE 5310: COMBUSTION FUNDAMENTALS

Design and analysis of a Scramjet combustion Chamber

Prediction of the Lift-off, Blow-out and Blow-off Stability Limits of Pure Hydrogen and Hydrogen/Hydrocarbon Mixture Jet Flames Wu, Y., Al-Rahbi, I. S.,

ME 475/675 Introduction to Combustion

ME 475/675 Introduction to Combustion

Design Space for Combustor

Chapter 5 (Mattingly) By: Ehsan Roohi

EXAMPLE 2 Find lengths in circles in a coordinate plane

EVERYTHING YOU NEED TO KNOW TO GET A GRADE C

CS 250, Discrete Structures, Fall 2014 Nitesh Saxena

Area Surface Area Volume

Presentation transcript:

ME 475/675 Introduction to Combustion Lecture 39

Announcements HW16 Ch. 9 (8, 10,12) Due Monday, 12/1/2013 Term Project (3% of grade) Nothing dangerous please! Instructions: Must meet with Rachel to discuss proposal before the end of Today If you chose not to perform project you will forfeit 3% of your grade Please inform us if that is your choice Times to meet with Rachel Green about projects Wednesdays, 11-3 pm HREL 306 Fridays, 1-3pmHREL 306 Mondays, 11-4 pm HREL 306 Schedule other times by ing

Burning Fuel Jet (Diffusion Flame)

Flame length (a measurable quantity)

Experimentally-Confirmed Numerical Solutions Inverse Gaussian error function “inverf” from Table 9.4

Slot Burners

Geometry and Flow Rate Dependence

Fuel Dependence

Stoichiometric Factors

Primary Aeration (of nozzle) Ambient

Fuel Dilution Ambient

Example 9.4 Design a natural-gas burner for a commercial cooking range that has a number of circular ports arranged in a circle. The circle diameter is constrained to be 160 mm (6.3 inch). The burner must deliver 2.2 kW at full load and operate with 40 percent primary aeration. For stable operation, the loading of than individual port should not exceed 10 W per mm 2 of port area. (see Fig for typical design constraints for natural-gas burners.) Also, the full-load flame height should not exceed 20 mm. Determine the number and the diameter of the ports.

Fuel Dependence

Stoichiometric Factors