A new method for measuring the pressure distribution on harmonically oscillating wings

Title

A new method for measuring the pressure distribution on harmonically oscillating wings

 Author

Bergh, H.

Institution

National Aerospace Laboratory NLR

 Date

1964-07-16

 Abstract

A method is described, enabling to measure the pressure distribution on oscillating wings with the aid of one pressure transducer, mounted inside a scanning valve. The scanning valve, located outside the testsection, is connected to the model orifices by equal pressure leads. Special measures are taken to simplify the correction procedure, necessary to eliminate the influence of the pressure leads. A short description of the equipment, developped to measure a large number of pressures automatically, is given. The usefulness of the technique is demonstrated by some examples.

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 Publisher

Nationaal Lucht- en Ruimtevaartlaboratorium

 Access restriction

Campus only

 Source

NLR MP 224

 Part of collection

Aerospace Engineering Reports

 Document type

report

 Rights

(c) 1964 National Aerospace Laboratory NLR
Files
PDF NLR-MP.224.pdf 23.1 MB
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