A Method for Determining the Pressure on the Surface of a Model during Aerodynamic Testing,
Abstract
In experimental aerodynamics the familiar method of pressure determination limits the test capabilities due to the need for positioning a large number of sensors on the model. The present method obtains a continuous pressure distribution on models having complex shapes by coating a nonheat-conducting model with two heat-indicating coatings having different time dependent critical temperatures.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 18, 1973
- Accession Number
- AD0769059
Entities
People
- D. V. Khalezov
- G. I. Maikapar
Organizations
- National Air and Space Intelligence Center