THERMODYNAMICS OF GAS FLOW
Abstract
Contents: Conservation of mass; Newton's second law of motion and the momentum equation; first law of thermodynamics; combination of the laws of thermodynamics and of fluid mechanics for incompressible fluid flow; the velocity of sound; total pressure and total temperature; nozzle design; nozzle operating characteristics; simple area flow; compressibility phenomena; normal shock wave; oblique shock wave; simple frictional flow; simple T sub o flow; supersonic diffusers; steadily moving shock wave.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1956
- Accession Number
- AD0605761
Entities
People
- D. H. Daley
Organizations
- Air Force Institute of Technology