Implementation of Vortex Cavities in a Turbojet Diffuser Sponsor: Williams International Progress Report 4 November 16, 2006 TEAM CRUISE CONTROL Michael.

Slides:

Advertisements

Similar presentations

Foundations of Engineering and Technology

Advertisements

1 Vacuum Pressure Calculations. 2 Vaccalc The program vaccalc was used for all calculations. The program required three pieces of information for each.

VORTEX GENERATOR FOR HYDRO TURBINE KARSON WONG JOHNSON NG SNEHIL RAISINGHANI Senior Project.

Simple Carburettor Fuel System for a Piston Engine

Pitot Stagnation Tubes Under Laminar Conditions *P7.24 Jace Benoit February 15, 2007.

Monday 27 July 2009 CloudSat. Tasks for All Begin documentation in force Dani assemble water table Check GUI compatibility with Mac Molly finish sphere.

Da’ Fuser Team Turbojet Diffuser Study Progress Report 3 Robby Swoish Mike Vostrizansky Ryan Wiltshire November 10, 2005.

Da’ Fuser Team Turbojet Diffuser Study Progress Report 2 Robby Swoish Mike Vostrizansky Ryan Wiltshire November 3, 2005.

Da’ Fuser Team Turbojet Diffuser Study Data Presentation Robby Swoish Mike Vostrizansky Ryan Wiltshire November 29, 2005.

G.Barber Tracker Update, Berkeley 10 Feb Tracker Progress Contents:- Station Space Frame Patch Panel / Vacuum Seal Light Guide Map Position of Degrader/Support.

Da’ Fuser Team Turbojet Diffuser Study Progress Report 4 Robby Swoish Mike Vostrizansky Ryan Wiltshire November 17, 2005.

The most important statistic of a diffuser is its efficiency. The efficiency is a measure of how well a diffuser re-expands air and how much pressure is.

Implementation of Vortex Cavities in a Turbojet Diffuser Sponsor: Williams International Progress Report 5 December 5, 2006 TEAM CRUISE CONTROL Michael.

Implementation of Vortex Cavities in a Turbojet Diffuser Sponsor: Williams International Progress Report 3 November 9, 2006 TEAM CRUISE CONTROL Michael.

Work progress Dalila AMMOUR Buoyant flow inside penetration cavity Numerical procedure: Code used: Code_Saturne V1.4.0 Model used actually: K-eps standard.

RFCC Module Tech Board Schedule Discussion Steve Virostek Lawrence Berkeley National Lab MICE CM25 at RAL November 4, 2009.

Progress Report 2 November 2nd, 2006 TEAM CRUISE CONTROL

Computational Engineering Physics Lab. CAViDS Consortium Hydraulic Line FSI For CAViDS Consortium Internal Use Only 1 10/02/2014 For CAViDS Consortium.

CAViDS Consortium Fan Drive CFD For CAViDS Consortium Internal Use Only 1 07/31/14 For CAViDS Consortium Internal Use Only Viscous Fan Drive 3D CFD Conjugate.

Powered by HEI involvement in European Structural Funds Monday, December 08, 2014.

Implementation of Vortex Cavities in a Turbojet Diffuser Sponsor: Williams International Progress Report 1 October 26, 2006 TEAM CRUISE CONTROL Michael.

Da’ Fuser Team Turbojet Diffuser Study Progress Report 1 Robby Swoish Mike Vostrizansky Ryan Wiltshire October 27, 2005.

Water Services Trust Fund Financial Support for Improved Access to Water and Sanitation Implementation of UPC Projects 1.

Physiologic Control Algorithms for Rotary Blood Pumps using Pressure Sensor Input Edward Bullister, Ph.D. Sanford Reich, Ph.D. APEX Medical, Inc. ISRP.

Design of a Rocket Engine Thrust Augmentation Ejector Nozzle By: Sepideh Jafarzadeh Mentor: Dr. Timothy Takahashi Arizona State University Ira A. Fulton.

1 Airflow based self-assembly of silicon chips on foils | 13 Air based self-assembly of silicon chips on foils Name:B. van Leeuwen Coach:Dr.Ir. M. Tichem.

Monsanto Utility Sprayer; Updating, Rebuilding, and Adapting Project Dan Murphy, Sam Nesbitt, David Ferguson, Andy Marchese April 20, 2006 Objectives:

CONSTRUCTION Andrea d'AURIA PH / DT-DI / GAS.

Booster Bias Supply and Cavity Upgrade November 16 th, 2011.

Developing an Effective Evaluation to Check for Understanding Part 2 Susan E. Schultz, Ph.D. Evaluation Consultant PARK Teachers.

Team E2-4 Kerry Memory Desiree’ Seay James Plott Savannah Harrison.

LASA Medium-β Cavity Progress Update Paolo Michelato 2 nd ESS Collaboration Meeting - SRF Elliptical Cavities 15 th December 2015.

Fundamental Skills The skills needed as a base for further development You will be better prepared to progress in the world of work when you can: Manage.

Name Next Spelling Word #1 Next Previous Spelling Word #2 Next.

Prototype Review November 20, 2006 Team Moondogs Chris Culver Rahul Kirtikar Elias Krauklis Christopher Sampson Michael Widerquist.

RunToShop 1: Project plan estimates for the end of the course.

1 Flight 0904 Update. 2 Flight manifest 13 New REPs are scheduled to test in Existing REPs testing in new territories 3 Existing REPs testing for.

Control Rod Nozzle Guide Tubes improved by 4 drilled holes. Model as two coaxial tubes of fluid connected by 4 holes. Two inlets at the bottom from the.

IBBelle: Status & Plans

BCP Analysis Update Thomas Jones 22/7/16.

Existing Prototype Test Facility (PTF) and planned Series Test Facility Schroeder, Claus Cryo-Review Darmstadt

TEAM AIRZOOKA FIVE MAE 101A Summer 1, 2011 Seungmin Go Young Jin Kim

Complementary ISTC Projects #3888, 3889p

PendoTECH- Technology Overview Presentation Prepared for Centocor

SPS cryogenic proximity equipment and SM18 validation

PCB Design and Construction

Lab Report MENG Tao Tsukuba 20,Oct.,2011

Water Services Trust Fund Financial Support for Improved Access to Water and Sanitation Implementation of UPC Projects & the Roles and Responsibilities.

National Laboratory Association

MGT 598 STUDY Education Your Life - mgt598study.com.

Subject Name: AIRCRAFT PROPULSION Subject Code: 10AE55

DCLL TBM Design Status, Current and future activities

Team A.W.E.S.O.M.- O 4000 February 13, 2007.

The World’s Most Awkward Roller Coaster: The Pipethon

Modular R.O.V for Sub-Sea Operations

5 × 7 = × 7 = 70 9 × 7 = CONNECTIONS IN 7 × TABLE

5 × 8 = 40 4 × 8 = 32 9 × 8 = CONNECTIONS IN 8 × TABLE

4 × 6 = 24 8 × 6 = 48 7 × 6 = CONNECTIONS IN 6 × TABLE

5 × 6 = 30 2 × 6 = 12 7 × 6 = CONNECTIONS IN 6 × TABLE

10 × 8 = 80 5 × 8 = 40 6 × 8 = CONNECTIONS IN 8 × TABLE MULTIPLICATION.

3 × 12 = 36 6 × 12 = 72 7 × 12 = CONNECTIONS IN 12 × TABLE

Mini – iTX Computer Case

Team P16228: Magnetically Levitated Propeller

5 × 12 = × 12 = × 12 = CONNECTIONS IN 12 × TABLE MULTIPLICATION.

Looking for Shot Blasting Machine manufacturer in India

6a - SSG on Climate Change and Water SCG meeting 5 November 2008 Marieke van Nood, Unit D.2, DG Environment, European Commission.

5 × 9 = 45 6 × 9 = 54 7 × 9 = CONNECTIONS IN 9 × TABLE

3 × 7 = 21 6 × 7 = 42 7 × 7 = CONNECTIONS IN 7 × TABLE

Presentation transcript:

Implementation of Vortex Cavities in a Turbojet Diffuser Sponsor: Williams International Progress Report 4 November 16, 2006 TEAM CRUISE CONTROL Michael Feldman Marvin Kong Nansi Xue

Table of Contents CFD with vortex cavity Test preparation progress

CFD on Diffuser with Vortex Cavity Previous analysis determined the flow separation location Further CFD done on diffuser with vortex cavity No feedback tubes implemented yet

CFD (with Vortex Cavities) Thinning of boundary layer when vortex cavities are implemented

Diffuser Components SLA model has been sent to Williams International, expected to receive the model on Monday or Tuesday New diffuser adapter has been constructed Final piece: requires a 6” PVC pipe to connect the adaptor to the vacuum inlet

Diffuser Components Pipe to be ordered from

Testing Set-up All major testing components have been accounted for Requires pitot tubes and epoxy to finish up experiment preparation Adaptor Nozzle Vacuum inletFlow speed regulator

Questions?