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NASA Lift Fan V/STOL Transport Technology Status
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English
Abstract
This paper is an overview of the status of lift fan transport technology. Selected results of recently completed NASA in-house and contractual research investigations are included within the general areas of lift fan transport design: propulsion, acoustics, integrated propulsion/airframe/aircraft control systems, piloted moving-base simulation, and aircraft aerodynamics. On-going NASA lift fan transport research is briefly summarized, and a possible next step in the overall program is suggested.
Authors
Citation
Deckert, W. and Evans, R., "NASA Lift Fan V/STOL Transport Technology Status," SAE Technical Paper 720856, 1972, https://doi.org/10.4271/720856.Also In
References
- McDonnell Aircraft Co. “Conceptual Design of a V/STOL Lift Fan Commercial Short Haul Transport.” Pending final report to NASA under contract NAS2-5499
- North American Rockwell “Conceptual Design Study of a V/STOL Lift Fan Commercial Short Haul Transport.” Pending final report to NASA under contract NAS2-6564
- The Boeing Co. “Conceptual Design Studies of Candidate V/STOL Lift Fan Commercial Short Haul Transport for 1980-1985.” Pending final report to NASA under contract NAS2-6563
- General Electric Co. “Remote Lift Fan Study Program.” Pending final report, NASA CR-120970
- General Electric Co. “Preliminary Design Study of Quiet Integral Fan Lift Engines for VTOL Transport Applications in the 80's.” Pending final report, NASA CR-120969
- Kirk Jerry V. Hall Leo P. Hodder Brent K. “Aerodynamics of Lift Fan V/STOL Aircraft.” NASA TM X-62, 086 September 1971