'Supersonic flow' presentation slideshows

MAE 5350: Gas Turbines

MAE 5350: Gas Turbines. Nozzles Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk. OVERVIEW: NOZZLES. Subsonic Aircraft: Usually a fixed area convergent nozzle is adequate Can be more complex for noise suppression

632 views • 62 slides

715 views • 54 slides

Shuxing Chen ? Fudan University ?

Shuxing Chen ? Fudan University ?. Mathematical Analysis of Supersonic flow past bodies. Since the twenty century the flight technology developed rapidly. Today different aircrafts with speed more than ten times of the sonic one have been designed. ???? ?????. ????????????.

565 views • 54 slides

MAE 4261: AIR-BREATHING ENGINES

MAE 4261: AIR-BREATHING ENGINES. Gas Turbine Engine Nozzles Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk. OVERVIEW: NOZZLES. Subsonic Aircraft: Usually a fixed area convergent nozzle is adequate Can be more complex for noise suppression

630 views • 44 slides

Compressibility

472 views • 32 slides

Combustion Team High Speed Combustion

Sara Esparza Cesar Olmedo Alonzo Perez. Combustion Team High Speed Combustion. Faculty Advisors:. Student Researchers:. Dr. Guillaume Dr. Wu Dr. Boussalis Dr. Liu Dr. Rad. Purpose. To achieve and sustain Mach 1.0 to 2.0 speed, induce mixing and sustain combustion for a duration.

367 views • 23 slides

Combustion Team Supersonic Combustion

Sara Esparza Cesar Olmedo Alonzo Perez. Combustion Team Supersonic Combustion. Faculty Advisors:. Student Researchers:. Dr. Guillaume Dr. Wu Dr. Boussalis Dr. Liu Dr. Rad. Purpose. To achieve and sustain Mach 1.0 to 2.0 speed, induce mixing and sustain combustion for a duration.

418 views • 22 slides

Combustion Team Supersonic Combustion

Sara Esparza Cesar Olmedo Alonzo Perez. Combustion Team Supersonic Combustion. Faculty Advisors:. Student Researchers:. Dr. Guillaume Dr. Wu Dr. Boussalis Dr. Liu Dr. Rad. Outline. Recent testing Shortened Combustion Chamber Determination of Mach Speed Schlieren

409 views • 18 slides

Thrust

Thrust. E80 Static Motor Test Spring 2009. Forces on a Rocket. http://www.grc.nasa.gov/WWW/K-12/rocket/rktth1.html. The Question. In the event of a crash landing of your rocket, what will be the effect on the instruments inside the rocket? (Translation) What is the velocity of impact?

496 views • 16 slides

Ch10 Conical Flow

1.27k views • 15 slides

Supersonic Conical Flow

Supersonic Conical Flow. In 2-D supersonic flow, shocks create abrupt changes in the flow which remain until another wave acts on it. In contrast, in 3-D or axi-symmetric supersonic flow, shock also exist, but flow properties may continue to vary after the shock.

697 views • 10 slides

What do we know about sound?

What do we know about sound?. Where does it come from?. Vibrating bodies Changing airflow Time-dependent heat sources Supersonic flow. 1. Biological receptors: Pressure changes on eardrums, skin 2. Technical receptors: microphone 3. Mechanical vibrations

148 views • 7 slides