Cover Image

Identification of XV-15 aeroelastic modes using frequency-domain methods /

Bibliographic Details
Main Author:	Acree, C. W.
Corporate Authors:	Ames Research Center, United States. Army Aviation Research and Technology Activity
Other Authors:	Tischler, Mark B. (Mark Brian), 1957-
Format:	Government Document Microform Book
Language:	English
Published:	Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center : US Army Aviation Systems Command, Aviation Research and Technology Activity ; [1989]
Series:	USAAVSCOM conference publication ; 89-A-001. NASA technical memorandum ; 101021.
Subjects:	Tilt rotor aircraft > Testing. Aeroelasticity. Curve fitting. Resonant frequencies. Tilting rotors. Vibration damping. XV-15 aircraft.
Online Access:	https://purl.fdlp.gov/GPO/LPS67457

Similar Items

The history of the XV-15 tilt rotor research aircraft : from concept to flight /
by: Maisel, Martin D.
Published: (2000)

Defining gas turbine engine performance requirements for the Large Civil TiltRotor (LCTR2) /
by: Snyder, Christopher A.
Published: (2013)

A CFD study of tilt rotor flowfields /
by: Fejtek, Ian
Published: (1989)

Airloads on bluff bodies, with application to the rotor-induced downloads on tilt-rotor aircraft /
Published: (1983)

Application of the wide-field shadowgraph technique to rotor wake visualization /
by: Norman, Tom
Published: (1989)

Variable-speed power-turbine research at Glenn Research Center /
Published: (2012)

Technology assessment for large vertical-lift transport tiltrotors /
by: Germanowski, Peter J.
Published: (2010)

Computational study of the impact of unsteadiness on the aerodynamic performance of a variable-speed power turbine /
by: Welch, Gerard E.
Published: (2012)

Variable-speed power-turbine for the large civil tilt rotor /
by: Suchezky, Mark
Published: (2012)

Aerodynamic measurements of a variable-speed power-turbine blade section in a transonic turbine cascade /
by: Flegel, Ashlie B.
Published: (2014)

Comprehensive modeling and analysis of rotorcraft variable speed propulsion system with coupled engine/transmission/rotor dynamics /
by: DeSmidt, Hans A.
Published: (2013)

Double helical gear performance results in high speed gear trains /
Published: (2010)

Gas turbine characteristics for a large civil tilt-rotor (LCTR) /
by: Snyder, Christopher A.
Published: (2010)

Gear design effects on the performance of high speed helical gear trains as used in aerospace drive systems /
by: Handschuh, Robert F.
Published: (2013)

Large Civil Tiltrotor (LCTR2) interior noise predictions due to turbulent boundary layer excitation /
by: Grosveld, Ferdinand W.
Published: (2013)

Summary of the Large Civil Tiltrotor (LCTR2) engine gearbox study /
Published: (2010)

Design study of propulsion and drive systems for the Large Civil TiltRotor (LCTR2) rotorcraft /
by: Robuck, Mark
Published: (2013)

An assessment of civil tiltrotor concept of operations in the next generation air transportation system /
by: Chung, William W.
Published: (2012)

Wind tunnel interference effects on tiltrotor testing using computational fluid dynamics /
by: Koning, Witold J. F.
Published: (2016)

Effects of gas turbine component performance on engine and rotary wing vehicle size and performance /
by: Herrick, Gregory P.
Published: (2010)

Assessment of aerodynamic challenges of a variable-speed power turbine for large civil tilt-rotor application /
by: Welch, Gerard E.
Published: (2010)

Compressor study to meet large civil tilt rotor engine requirements /
by: Veres, Joseph P.
Published: (2009)

Study and sub-system optimization of propulsion and drive systems for the Large Civil TiltRotor (LCTR2) rotorcraft /
by: Robuck, Mark
Published: (2013)

Computational assessment of the aerodynamic performance of a variable-speed power turbine for large civil tilt-rotor application /
by: Welch, Gerard E.
Published: (2011)

NDARC : NASA Design and Analysis of Rotorcraft /
by: Johnson, Wayne, 1946-
Published: (2009)

Variable-speed simulation of a dual-clutch gearbox tiltrotor driveline /
Published: (2012)

Ground-simulation investigations of VTOL airworthiness criteria for terminal-area operations /
Published: (1990)

Potential use of tiltrotor aircraft in Canadian aviation /
by: Gazdag, Denyse
Published: (1990)

Multipoint design and optimization of a turboshaft engine for a tiltwing turboelectric vertical takeoff landing air taxi /
by: Chapman, Jeffryes W.
Published: (2019)

Quiet mode for nonlinear rotor models /
by: McFarland, R. E.
Published: (1990)

Fuselage upwash effects on RSRA rotor systems /
by: Cowan, J.
Published: (1985)

The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover /
by: Bousman, William G.
Published: (1990)

Estimation of dynamic rotor loads for the rotor systems research aircraft : methodology development and validation /
by: Du Val, R. W.
Published: (1985)

Aeromechanical stability of a hingeless rotor in hover and forward flight : analysis and wind tunnel tests /
by: Yeager, William T., et al.
Published: (1983)

Calculated performance of the NASA Lewis icing research tunnel /
by: Viterna, Larry A.
Published: (1991)

SSME interstage seal research : progress report /
by: Childs, Dara W.
Published: (1984)

Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver /
by: Bakhle, Milind A.
Published: (1996)

The effect of modified control limits on the performance of a generic commercial aircraft engine /
Published: (2012)

Ultrasonic resonance spectroscopy of composite rims for flywheel rotors /
by: Harmon, Laura M., et al.
Published: (2002)

Ultrasonic resonance spectroscopy of composite rims for flywheel rotors /
by: Harmon, Laura M.
Published: (2002)