Materials Evaluation for Aircraft Blast and Helicopter Downwash Protection.
Abstract
This investigation was conducted to evaluate materials and develop construction techniques for the rapid protection of airfield and heliport shoulders and overrun areas against hot engine blast and rotor downwash with ground air velocities up to 125 mph using existing materials. The objective was accomplished by a series of jet engine exhaust blasts impinging on a number of treated test areas. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1975
- Accession Number
- ADA121761
Entities
People
- Grady W. Leese
- James W. Carr