Determination of Optimum Parameters of the Means Used to Protect the Compartments of an Aircraft from Aerodynamic Heat at High Speeds and during a Prolonged Flight,
Abstract
Optimum parameters of the means used to protect the aircraft compartments from aerodynamic heat are determined. The thermal conductivity coefficient is expressed in the form of a linear temperature function when studying the external and internal heat insulators. Coupling equations are used in computations using electronic digital computer. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 05, 1973
- Accession Number
- AD0754606
Entities
People
- A. A. Kobylyanskii
- F. G. Yasinskii
Organizations
- National Air and Space Intelligence Center