Works matching IS 00028711 AND DT 2017 AND VI 62 AND IP 4

Results: 12

Practical Methods for Aircraft and Rotorcraft Flight Control Design: An Optimization Based Approach.

Published in:

2017

By:

Hodgkinson, John

Publication type:

Book Review

Formation Control of a Rotorcraft Multilift System.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042011

By:

Enciu, Jacob;
Horn, Joseph F.;
Langelaan, Jacob W.

Publication type:

Article

Influence of Dynamic Inflow States on Coupled Rotor Fuselage Modes.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042010

By:

Nair, Salini S.;
Mohan, Ranjith;
Gaonkar, Gopal

Publication type:

Article

Modeling and Design of a Tailboom Vibration Absorber Using Fluidic Flexible Matrix Composite Tubes.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042009

By:

Miura, Kentaro;
Smith, Edward C.;
Rahn, Christopher D.

Publication type:

Article

Performance Qualification of an On-Board Model-Based Diagnostic System for Fatigue Crack Monitoring.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042008

By:

Sbarufatti, C.;
Giglio, M.

Publication type:

Article

System Identification and Controller Optimization of a Quadrotor Unmanned Aerial Vehicle in Hover.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042007

By:

Wei Wei;
Tischler, Mark B.;
Cohen, Kelly

Publication type:

Article

A Virtual Pilot Algorithm for Synthetic HUMS Data Generation.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042006

By:

Fowler, Lee;
Rogers, Jonathan;
Sarkar, Subhasis;
Iyyer, Nagaraja

Publication type:

Article

Adjoint-Based Aeroacoustic Design-Optimization of Flexible Rotors in Forward Flight.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042005

By:

Fabiano, Enrico;
Mavriplis, Dimitri

Publication type:

Article

An Efficient Approach for the Simulation and On-Blade Control of Helicopter Noise and the Impact on Vibration.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042004

By:

Chia, Miang H.;
Padthe, Ashwani K.;
Duraisamy, Karthik;
Friedmann, Peretz P.

Publication type:

Article

Analysis of the TurbulentWake Generated by a Micro Air Vehicle Hovering near the Ground with a Lattice Boltzmann Method.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042003

By:

Gourdain, Nicolas;
Singh, Deepali;
Jardin, Thierry;
Prothin, Sébastien

Publication type:

Article

The First Wind Tunnel Test of the Multiple Swashplate System: Test Procedure and Principal Results.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042002

By:

Küfmann, Philip M.;
Bartels, Rainer;
van der Wall, Berend G.;
Schneider, Oliver;
Holthusen, Hermann;
Gomes, Jorge

Publication type:

Article

From Aeroacoustics Basic Research to a Modern Low-Noise Rotor Blade.

Published in:

Journal of the American Helicopter Society, 2017, v. 62, n. 4, p. 1, doi. 10.4050/JAHS.62.042001

By:

van der Wall, Berend G.;
Kessler, Christoph;
Delrieux, Yves;
Beaumier, Philippe;
Gervais, Marc;
Hirsch, Jean-François;
Pengel, Kurt;
Crozier, Pascal

Publication type:

Article