Instrumentation system for determining flow stagnation points

• US 5,218,863 A
• Filed: 10/28/1991
• Issued: 06/15/1993
• Est. Priority Date: 10/28/1991
• Status: Expired due to Term

• Current Assignee: Tao of Systems Integration, Inc.
• Original Assignee: Analytical Services And Materials, Inc.
• Inventors: Mangalam, Siva M.
• Primary Examiner(s): WOODIEL, DONALD
• Application Number:
  US07/783,217
• Time in Patent Office: 596 Days
• Field of Search: 73/147, 73/180, 73/178 R, 73/178 T, 73/178 H, 244/204.11, 244/203, 244/204, 244/130
• US Class Current: 73/147
• CPC Class Codes: G01M 9/065 dealing with flow
• CPC Class Codes: G01P 5/12 using variation of resistance of a heated conductor

Abstract

A method and portable microcomputer-based system for determining flow field stagnation points are disclosed. The apparatus uses hot film sensors wrapped around the leading edge of an airfoil to measure boundary layer oscillations. A plurality of sensor signals are provided which may be selected in groups. Signals from sensors in any group are read simultaneously. The signals are then converted to digital form and displayed on the video display of a microcomputer. Points of airflow stagnation are characterized by a doubling in frequency or other discrete harmonics and by a reversing of the phase of oscillations. Those points are identified by displaying and comparing signals from different sensor locations on a video display.

Claims

1. A method for determining flow stagnation points on an airfoil comprising the steps of:

(a) providing an airfoil located in a flow field;

(b) locating a plurality of sensors on the surface of said airflow, said sensor location extending from the under surface around the leading edge to the upper surface;

(c) sensing, from said plurality of sensors, simultaneous frequency oscillations in boundary layer flow;

(d) generating output signals corresponding to the sensed frequency oscillations; and

(e) comparing output signals to determine locations having both phase reversal and a higher frequency harmonics, such locations being flow stagnation points.

2. An apparatus for determining stagnation points on an airfoil comprising:

(a) a plurality of multi-element hot film sensors located on an airfoil surface at the leading edge and wrapping around the leading edge thereby covering both upper and lower forward airfoil surfaces in the region of flow stagnation;

(b) a plurality of sensor circuit cards electrically connected to said multi-element hot film sensors;

(c) a multiplexer circuit card electrically connected to said sensor circuit cards;

(d) an amplifier and signal conditioner circuit card electrically connected to said multiplexer circuit card;

(e) an interface circuit card electrically connected to said amplifier and signal conditioner card;

(f) a microcomputer containing said interface circuit card in an internal expansion slot; and

(g) software for selecting sensors and displaying sensor signals generated by frequency fluctuations in heat transfer.

3. An apparatus for determining stagnation points on an airfoil comprising:

(a) means for sensing boundary layer oscillations and providing signals thereof;

(b) means for selecting and filtering said sensor signals;

(c) means for processing sensor signals to obtain frequency characteristics; and

(d) means for displaying frequency characteristics including phase and frequency of oscillation.

4. An apparatus for determining stagnation points as in claim 3 wherein said means for sensing boundary layer oscillations comprise a plurality of multi-element hot film sensors.

5. Multi-element hot film sensors as in claim 4 wherein each sensor comprises a plurality nickel sensor elements affixed to a non-conductive substrate.

6. An apparatus for determining stagnation points as in claim 3 wherein said means for sensing boundary layer oscillations further comprise a plurality of thermal anemometer means.

7. An apparatus for determining stagnation points as in claim 3 wherein said means for selecting and filtering said sensor signals comprises a software-controlled multiplexer circuit card.

8. An apparatus for determining stagnation points as in claim 3 wherein said means for processing said sensor signals further comprises an amplifier and signal conditioner circuit card.

9. An apparatus for determining stagnation points as in claim 3 wherein said means for processing sensor signals comprises a microcomputer having an internally-mounted interface circuit card for receiving selected sensor signals.

10. An interface circuit card as in claim 9 wherein said interface circuit card comprises an analog-to-digital converter having eight independent channels thereby allowing simultaneous reception of eight separate signals.

11. An apparatus for determining stagnation points as in claim 3 wherein said means for displaying frequency characteristics further comprises a software program.

12. An apparatus for determining stagnation points as in claim 3 wherein means for displaying frequency characteristics further comprise a video display of phase reversal signatures thereby identifying stagnation locations.