Development of a rotorcraft. Propulsion dynamics interface analysis, volume 2.
- Hull, R.
- Aug 1, 1982.
- Physical Description:
- 1 electronic document
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- A study was conducted to establish a coupled rotor/propulsion analysis that would be applicable to a wide range of rotorcraft systems. The effort included the following tasks: (1) development of a model structure suitable for simulating a wide range of rotorcraft configurations; (2) defined a methodology for parameterizing the model structure to represent a particular rotorcraft; (3) constructing a nonlinear coupled rotor/propulsion model as a test case to use in analyzing coupled system dynamics; and (4) an attempt to develop a mostly linear coupled model derived from the complete nonlinear simulations. Documentation of the computer models developed is presented.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19820024493., Accession ID: 82N32369., NASA-CR-166381., and NAS 1.26:166381.
- No Copyright.
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