Stability of helicopters
Resource Information
The concept Stability of helicopters represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
The Resource
Stability of helicopters
Resource Information
The concept Stability of helicopters represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
- Label
- Stability of helicopters
- Authority link
- (EG-IN)646608
43 Items that share the Concept Stability of helicopters
Context
Context of Stability of helicoptersSubject of
- A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications
- Active arm (external cargo) stabilization system flight demonstration
- Advanced electrofluidic servovalve development
- Advanced fluidic temperature studies
- Aeroelastic analysis for rotorcraft in flight or in a wind tunnel
- Aeroelastic effects in multirotor vehicles, Part II--methods of solution and results illustrating coupled rotor/body aeromechanical stability
- Aeroelastic rotor stability analysis
- An assessment of the capability to calculate tilting prop-rotor aircraft performance, loads, and stability
- Analysis of stability contributions of high dihedral V-trails
- Approval basis for automatic stabilization equipment (ASE) installations in rotorcraft
- Comparison of analytical and flight test identified aerodynamic derivatives for a tandem-rotor transport helicopter
- Computer simulation of a single pilot flying a modern high-performance helicopter
- Computer simulation of multiple pilots flying a modern high performance helicopter
- Control of a human-powered helicopter in hover
- Demonstration of frequency-sweep testing technique using a Bell 214-ST helicopter
- Description of the VTOL approach and landing technology (VALT) Ch-47 research system
- Design and analysis of an active jet control system for helicopter sling loads
- Design, development, and flight demonstration of the loads and stability characteristics of a bearingless main rotor
- Development and evaluation of an inverse solution technique for studying helicopter maneuverability and agility
- Development and flight test of an advanced hydrofluidic stabilization system
- Developments in helicopter tail boom strake applications in the United States
- Documentation of helicopter aeroelastic stability analysis computer program (HASTA)
- Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft
- Engine/airframe/drive train dynamic interface documentation
- Fixed gain and adaptive techniques for rotorcraft vibration control
- Frequency-response identification of XV-15 tilt-rotor aircraft dynamics
- Helicopter dynamic rollover
- Helicopter rotor blade design for minimum vibration
- Helicopter vibration suppression using simple pendulum absorbers on the rotor blade
- Hydrofluidic stability augmentation system (HYSAS): : operational suitability demonstration | final report for period March 1973-March 1977
- Improvement of helicopter attitude stability by active control of the conventional swash plate
- Influence of dynamic inflow on the helicopter vertical response
- Interior noise and vibration measurements on operational military helicopters and comparisons with various ride quality criteria
- Investigation of a low-cost servoactuator for HYSAS
- Lateral rollover protection concepts
- Practical optimal flight control system design for helicopter aircraft
- Predesign of the second generation comprehensive helicopter analysis system
- Predesign of the second-generation comprehensive helicopter analysis system
- Review of airworthiness standards for certification of helicopters for instrument flight rules (IFR) operation
- Rotorcraft flight simulation computer program C81 with DATAMAP interface
- Self-tuning regulators for multicyclic control of helicopter vibration
- Stability and control of airplanes and helicopters
- Study to eliminate ground resonance using active controls
Embed (Experimental)
Settings
Select options that apply then copy and paste the RDF/HTML data fragment to include in your application
Embed this data in a secure (HTTPS) page:
Layout options:
Include data citation:
<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/D91w94u8-dY/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/D91w94u8-dY/">Stability of helicopters</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
Note: Adjust the width and height settings defined in the RDF/HTML code fragment to best match your requirements
Preview
Cite Data - Experimental
Data Citation of the Concept Stability of helicopters
Copy and paste the following RDF/HTML data fragment to cite this resource
<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/D91w94u8-dY/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/D91w94u8-dY/">Stability of helicopters</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
