Revitalising advanced rotorcraft research – and the compound helicopter
@article{Ormiston2016RevitalisingAR, title={Revitalising advanced rotorcraft research – and the compound helicopter}, author={Robert A. Ormiston}, journal={The Aeronautical Journal}, year={2016}, volume={120}, pages={83 - 129} }
PREFACE I was honoured to have been selected to deliver the 35th Nikolsky Honorary Lecture. My graduate education at Princeton University owed much to the influence of Alexander A. Nikolsky, the second faculty member appointed to the Princeton Aeronautical Engineering Department in 1943(1). I arrived in 1963, only months after he passed away, but the memory of his presence was still vivid in the minds of his students and colleagues, as well as the professors who introduced me to rotorcraft(2,3…
12 Citations
Design and aeromechanics investigation of compound helicopters
- EngineeringAerospace Science and Technology
- 2019
Study on the lift and propulsive force shares to improve the flight performance of a compound helicopter
- Engineering
- 2021
Improved rotor aeromechanics predictions using a fluid structure interaction approach
- Engineering
- 2018
An Experimental Study on Blade Deformation of Coaxial Rotor System Using SPR(Stereo Pattern Recognition) Technique
- Engineering
- 2020
These days, the coaxial rotor system is used for various purposes like UAVs, Mars exploration helicopters, and the next-generation high-speed rotorcraft. A number of research projects on aerodynamic…
Vibratory load predictions of a high-advance-ratio coaxial rotor system validated by wind tunnel tests
- Engineering
- 2017
MODAL CHARACTERISATION OF A ROTOR/PROPELLER RIG FOR TIP-MACH SCALED WIND TUNNEL TESTING
- Engineering
- 2021
An advanced rotor and propeller rig for tip Mach-scaled wind tunnel testing is the subject of dynamic analysis presented in this paper. Experimental modal analysis and finite element method are used…
High-fidelity numerical investigations of rotor-propeller aerodynamic interactions
- EngineeringAerospace Science and Technology
- 2022
Toward Vehicle-Level Optimization of Compound Rotorcraft Aerodynamics
- EngineeringAIAA Journal
- 2021
Robust Full-Envelope Flight Control Design for an eVTOL Vehicle
- Computer ScienceAIAA Scitech 2021 Forum
- 2020
References
SHOWING 1-10 OF 101 REFERENCES
How Dynamic Inflow Survives in the Competitive World of Rotorcraft Aerodynamics
- Physics
- 2009
Dynamic wake models have found a firm place in rotary-wing analysis since their inception in the 1950s, proliferation in the 1970s, and maturation in the 1990s. They have maintained their usefulness,…
Aeromechanics Analysis of a Heavy Lift Slowed-Rotor Compound Helicopter
- Engineering
- 2007
A heavy lift slowed-rotor tandem compound helicopter was designed as a part of the NASA heavy lift rotorcraft systems investigation. The vehicle is required to carry 120 passengers over a range of…
Optimum Design of a Compound Helicopter
- Engineering
- 2009
A design and aeromechanics investigation was conducted for a 100,000-lb compound helicopter with a single main rotor, which is to cruise at 250 knots at 4000 ft/95 deg F condition. Performance,…
Rotorcraft Airloads Measurements Extraordinary Costs, Extraordinary Benefits
- Engineering
- 2011
Abstract : The first airloads measurements were made in the 1950s at NACA Langley on a 15.3-foot-diameter model rotor, stimulated by the invention of miniaturized pressure transducers. The inability…
Dynamics of tilting proprotor aircraft in cruise flight
- Engineering
- 1974
A nine degree-of-freedom theoretical model is developed for investigations of the dynamics of a proprotor operating in high inflow axial flight on a cantilever wing. The basic characteristics of the…
WIND TUNNEL INVESTIGATION OF SEMIRIGID FULL-SCALE ROTORS OPERATING AT HIGH ADVANCE RATIOS
- Engineering
- 1969
Abstract : A UH-1B 44-foot-diameter rotor having reduced-thickness tips was evaluated in a range of Mach numbers up to 0.94 and advance ratios of up to 0. 52. Additionally, UH-1D rotor blades reduced…
Review of Rotor Loads Prediction with the Emergence of Rotorcraft CFD
- Engineering
- 2007
This paper reviews the state of the art in helicopter rotor loads prediction using Computational Fluid Dynamics (CFD) and Computational Structural Dynamics (CSD) coupling. The application of CFD to…
Overview of the Helios Version 2.0 Computational Platform for Rotorcraft Simulations
- Computer Science
- 2011
The capabilities and development of the Helios version 2.0, or Shasta, software for rotary wing simulations, include off-body adaptive mesh refinement and the ability to handle multiple interacting rotorcraft components such as the fuselage, rotors, flaps and stores.
Putting the Aero Back into Aeroelasticity
- Engineering
- 1999
The lack of progress in understanding the physics of rotorcraft loads and vibration over the last 30 years is addressed in this paper. As befits this extraordinarily difficult problem, the reasons…
Design Considerations for Bearingless Rotor Hubs
- Engineering
- 1983
Abstract : Five studies were performed under contract for concept definition of the Integrated Technology Rotor/Flight Research Rotor (ITR/FRR) Project. The purpose of these studies was to examine…