NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Performance and loads data from a hover test of a full-scale XV-15 rotorA hover test of a full-scale XV-15 rotor was conducted at the Outdoor Aerodynamic Research Facility at Ames Research Center. The primary objective of the test was to obtain accurate measurements of the hover performance of the original, metal-blade XV-15 rotor system. Data were acquired for rotor tip Mach numbers ranging from 0.60 to 0.73. This report presents data on rotor performance, rotor wake downwash velocities, and rotor loads.
Document ID
19860005773
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Felker, F. F. (NASA Ames Research Center Moffett Field, CA, United States)
Betzina, M. D. (NASA Ames Research Center Moffett Field, CA, United States)
Signor, D. B. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:86833
NASA-TM-86833
REPT-85404
Report Number: NAS 1.15:86833
Report Number: NASA-TM-86833
Report Number: REPT-85404
Accession Number
86N15243
Funding Number(s)
PROJECT: RTOP 536-02-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available