NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Flight Testing the Rotor Systems Research Aircraft (RSRA)In the late 1960s, efforts to advance the state-of-the-art in rotor systems technology indicated a significant gap existed between our ability to accurately predict the characteristics of a complex rotor system and the results obtained through flight verification. Even full scale wind tunnel efforts proved inaccurate because of the complex nature of a rotating, maneuvering rotor system. The key element missing, which prevented significant advances, was our inability to precisely measure the exact rotor state as a function of time and flight condition. Two Rotor Research Aircraft (RSRA) were designed as pure research aircraft and dedicated rotor test vehicles whose function is to fill the gap between theory, wind tunnel testing, and flight verification. The two aircraft, the development of the piloting techniques required to safely fly the compound helicopter, the government flight testing accomplished to date, and proposed future research programs.
Document ID
19840005109
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hall, G. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Merrill, R. K.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
USAAVRADCOM-TM-83-A-1
NAS 1.15:85852
A-9510
NASA-TM-85852
Report Number: USAAVRADCOM-TM-83-A-1
Report Number: NAS 1.15:85852
Report Number: A-9510
Report Number: NASA-TM-85852
Accession Number
84N13177
Funding Number(s)
PROJECT: RTOP 532-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available