- Additional Authors
- Description
- iv, 56 p. : ill.
- Summary
- In comparison to turbo-prop applications, the Prop-Fan is designed to operate in a significantly higher range of aircraft flight speeds. Two concerns arise regarding operation at very high speeds: aerodynamic performance and noise generation. This data package covers both topics over a broad range of operating conditions for the eight (8) bladed SR-7L Prop-Fan. Operating conditions covered are: Flight Mach Number 0-0.85; blade tip speed 600-800 ft/sec; and cruise power loading 20-40 SHP/D2. Prop-Fan weight and weight scaling estimates are also included.
- Series Statement
- NASA contractor report ; CR-174782
- Uniform Title
- NASA contractor report ; NASA CR-174782.
- Subject
- Note
- "February 1985."
- "SP-06A83."
- Author affiliation: Hamilton Standard, Windsor Locks, CT.
- Reproduction (note)
- Funding (note)
- Call Number
- GPO Microfiche NAS 1.26:174782
- OCLC
- marcive263074695
- Author
Parzych, David J.
- Title
Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984 [microform] / D. Parzych, [S. Cohen, A. Shenkman].
- Imprint
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
- Series
NASA contractor report ; CR-174782
NASA contractor report ; NASA CR-174782.
- Funding
NASA contract NAS 3-23051
- Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1985. 1 microfiche : negative.
- Added Author
Cohen, S.
Shenkman, A.
United States. National Aeronautics and Space Administration.
United Technologies Corporation. Hamilton Standard Division.
- Other Form:
Online version: Parzych, David J. Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984. (OCoLC)708253427
- Gpo Item No.
0830-H-14 (MF)
- Sudoc No.
NAS 1.26:174782