SYSTEM AND METHOD FOR MEASURING EXHAUST FLOW VELOCITY OF SUPERSONIC NOZZLES

• US 20170336431A1
• Filed: 05/19/2017
• Published: 11/23/2017
• Est. Priority Date: 05/19/2016
• Status: Abandoned Application

• Current Assignee: Purdue Research Foundation (The Trustees of Purdue University (d/b/a Purdue University))
• Original Assignee: Purdue Research Foundation (The Trustees of Purdue University (d/b/a Purdue University))
• Inventors: Willits, Jared D., Pourpoint, Timothee L.
• Application Number:
  US15/600,700
• Publication Number:
  US 20170336431A1
• Time in Patent Office: Days
• CPC Class Codes: G01P 5/26 by measuring the direct influence of the streaming fluid on the properties of a detecting optical wave

Abstract

A system for measuring supersonic nozzle exhaust flow, comprising a seeding module, an optics module configured to direct an optical signal from the supersonic nozzle, and a streak camera. The streak camera is optically connected to the optical signal, the streak camera configured to image the path of the seed particles traveling in the nozzle exhaust flow. The seeding module includes a seed particle container and a seed particle injector configured to inject seed particles into a supersonic nozzle flow. The streak camera comprises a photocathode, a sweep module, a micro-channel plate, a phosphor screen, and a charged coupled imaging device.

Claims

1. A system for measuring supersonic nozzle exhaust flow, comprising:

a seeding module, the seeding module having a seed particle container and a seed particle injector configured to inject seed particles into a supersonic nozzle flow;

an optics module configured to direct an optical signal from the supersonic nozzle; and

a streak camera optically connected to the optical signal, the streak camera configured to image the path of the seed particles traveling in the nozzle exhaust flow.

2. The system of claim 1, wherein the seed particles comprise TiO₂.

3. The system of claim 1, wherein the seed particles comprise SiC.

4. The system of claim 1, wherein the nozzle is a supersonic rocket nozzle.

5. The system of claim 1, wherein the streak camera comprises a photocathode, a streak tube, a sweep module which adjust an electric field inside the streak tube to change the direction of electrons being output from the photocathode, a micro-channel plate which multiplies the electrons, a phosphor screen which receives the electrons and converts them to photons, and a charged coupled imaging device which senses the photons to form an image.

6. A method for measuring supersonic nozzle exhaust flow, comprising:

injecting seeded particles into a supersonic exhaust flow using a seeding module, the seeding module having a seed particle container and a seed particle injector configured to inject seed particles into the supersonic nozzle flow;

directing an optical signal from the flow via an optics module to a streak camera optically connected to the optical signal, the streak camera configured to image the path of the seed particles traveling in the nozzle exhaust flow.

7. The method of claim 6, wherein the seed particles comprise TiO₂.

8. The method of claim 6, wherein the seed particles comprise SiC.

9. The method of claim 6, wherein the nozzle is a supersonic rocket nozzle.

10. The method of claim 6, wherein the streak camera comprises a photocathode, a streak tube, a sweep module which adjust an electric field inside the streak tube to change the direction of electrons being output from the photocathode, a micro-channel plate which multiplies the electrons, a phosphor screen which receives the electrons and converts them to photons, and a charged coupled imaging device which senses the photons to form an image.