A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients.

Bibliographic Details

Main Author:	Whitmore, Stephen A.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Other Authors:	Petersen, Brian J., Scott, David D.
Format:	Government Document Book
Language:	English
Published:	[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; 1996.
Series:	NASA technical memorandum ; 4728.
Subjects:	Continuum flow. DYNAMIC MODELS. Hypersonics. Knudsen flow. Navier-Stokes equation. Pressure sensors. Rarefied gas dynamics.