Tunnel utilizing US Navy airship as stable model carriage developed by Subsonic Aerodynamics Laboratory of Princeton Univ is shown to give accurate, repeatable data for variety of configurations; details of ZS2G-1 used in initial feasibility studies, and ZPG-2 airship having increased endurance and capability; results with respect to velocity survey, vibration level, adaptability of mounting system, available power supply, ease of calibration, and access to model and ease of testing.
Navy's flying wind tunnel
Aerospace Eng
Aerospace Engineering ; 20 , n 3
1961
4 pages
Article (Journal)
English
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