Method for applying turbulators to wind tunnel models

• US 4,537,647 A
• Filed: 10/06/1982
• Issued: 08/27/1985
• Est. Priority Date: 10/06/1982
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Foster, Clark B.
• Primary Examiner(s): Kimlin, Edward
• Assistant Examiner(s): FALASCO, LOUIS V
• Application Number:
  US06/433,189
• Time in Patent Office: 1,056 Days
• Field of Search: 264/313, 264/297, 264/251, 264/264, 427/282, 427/272, 156/231, 156/232, 156/238, 156/249, 156/245, 156/247, 156/289, 156/307.7, 156/303, 156/344, 156/71, 244/119, 244/4 A, 244/132, 46/76 R, 46/79, 46/74, 73/147, 73/583, 73/802, 73/804, 73/861.32
• US Class Current: 156/245
• CPC Class Codes: B05D 1/32 using means for protecting parts of a surface not to be coated, e.g. using stencils, resists
• CPC Class Codes: B29C 67/08 Screen moulding, e.g. forcing the moulding material through a perforated screen on to a moulding surface
• CPC Class Codes: B29K 2063/00 Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
• CPC Class Codes: B29L 2031/3076 Aircrafts blades, propellers B29L2031/08
• CPC Class Codes: B29L 2031/40 Test specimens ; Models, e.g. model cars mannequins B29L2031/7028; Probes
• CPC Class Codes: G01M 9/06 Measuring arrangements specially adapted for aerodynamic testing
• CPC Class Codes: G09B 23/12 of liquids or gases

Abstract

A method for forming turbulators on scale model airplanes used in wind tunnel testing for accurately simulating a transition point on the model surface equivalent to that produced on the full scale airplane. The transition point is where the boundary layer airflow goes from a laminar airflow condition to a turbulent airflow condition. The method relates to applying a perforated tape mask (14) to the model surface (12) at a predetermined location and filling the perforations (15) with a fast cure epoxy (17). After the epoxy has cure hardened, the tape mask (14) is peeled off in the direction of the arrow (16), leaving a series of in situ formed disk turbulators (10) which function to produce the transition point on the model surface.

Claims

1. A method for forming turbulators in situ on the surface of a scale model airfoil used in wind tunnel testing, comprising the steps of:

forming a mold by applying an adhesive backed tape stencil having a series of circular apertures, to a predetermined location on said airfoil;

filling the apertures in said tape stencil with an epoxy resin;

leveling the epoxy resin with the surface of said tape stencil;

cure hardening said epoxy resin;

removing said tape stencil from said airfoil and leaving in situ formed epoxy disk turbulators on said airfoil;

predetermining a thickness of said tape stencil for substantially producing a height of the epoxy disk turbulators which protrudes into free airstream flow in the wind tunnel during testing of said scale model airfoil for producing a transition point on said airfoil.

2. The method set forth in claim 1, including:

spacing the series of circular apertures in said tape stencil such that the distance between them is within the range of from approximately one diameter to two diameters.

3. In a method for forming turbulators as recited in claim 1, including:

applying a release agent line on the surface of said scale model airfoil prior to the application of said tape stencil; and

positioning the series of circular apertures of said tape stencil over said release agent line which functions to decrease the bond area between the in situ formed epoxy disk turbulators and the model surface, thereby making said turbulators more easily removable without damage to the model surface.

4. A method for forming turbulators on an aerodynamic scale model used in wind tunnel testing to simulate a transition point of laminar to turbulent airflow occurring on a full scale aerodynamic craft, comprising the steps of:

forming a mold by applying a tape mask having a series of circular perforations, to a predetermined location on said model;

filling the series of circular perforations in said tape mask with a cure hardening epoxy resin liquid;

removing excess epoxy resin to precisely limit epoxy filled perforations to a surface level of said tape mask;

cure hardening said epoxy resin;

peeling off said tape mask after the epoxy resin has cure hardened and leaving a series of in situ formed epoxy disk turbulators on said model;

predetermining a thickness of said tape mask for substantially producing a height of epoxy disk turbulators which protrude into free airstream flow and function to produce a transition point on the surface of said model during wind testing thereof.

5. The method set forth in claim 4, including:

spacing the series of circular perforations in said tape mask such that the distance between them is within the range of from approximately one diameter to two diameters.

6. In a method for forming turbulators as recited in claim 4, including:

applying a release agent line on the surface of said scale model prior to the application of said tape mask; and

positioning the series of circular perforations of said tape mask over said release agent line which functions to decrease the bond area between the in situ formed epoxy disk turbulators and the model surface, thereby making said turbulators more easily removable without damage to the model surface.