Determination of the Energy Performance of a Helicopter in a Hover

doi 10.21495/91-8-121
Full Text
Abstract

Available in full text

Date
Authors

Unknown

Publisher

Institute of Theoretical and Applied Mechanics of the Czech Academy of Sciences

Related search

Unstructured Mesh Navier-Stokes Calculations of the Flow Field of a Helicopter Rotor in Hover

Journal of the American Helicopter Society
2002English

Gust Response Analysis for Helicopter Rotors in the Hover and Forward Flights

Shock and Vibration
Mechanics of MaterialsGeotechnical EngineeringCondensed Matter PhysicsMechanical EngineeringCivilEngineering GeologyStructural Engineering
2017English

Flowfield Analysis of Modern Helicopter Rotors in Hover by Navier‐Stokes Method

Journal of the American Helicopter Society
1993English

Performance Enhancement of Rotors in Hover Using Fixed Gurney Flaps

2017English

Validation of the Steady-State Hover Formulation for Accurate Performance Predictions

AIAA Journal
Aerospace Engineering
2019English

Investigation of the Performance of Multiple Modeling and Control Approach Using a Laboratory Helicopter

International Journal of Computer and Electrical Engineering
2010English

The Near Field Pressure of a Small-Scale Rotor During Hover.

2010English

Examining the Stability Derivatives of a Compound Helicopter

Aeronautical Journal
Aerospace Engineering
2016English

Determination of the Energy Landscape of Pd12Pt1 Using a Combined Genetic Algorithm and Threshold Energy Method

RSC Advances
ChemistryChemical Engineering
2013English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy