Aircraft configurations
Resource Information
The concept Aircraft configurations represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
The Resource
Aircraft configurations
Resource Information
The concept Aircraft configurations represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
- Label
- Aircraft configurations
- Source
- nasat
54 Items that share the Concept Aircraft configurations
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- Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow
- 4D dynamic required navigation performance final report
- A comparison of interactional aerodynamics methods for a helicopter in low speed flight
- A modeling technique for STOVL ejector and volume dynamics
- A user's manual for ROTTILT solver : tiltrotor fountain flow field prediction
- A user's manual for the method of moments Aircraft Modeling Code (AMC)
- Advanced Rotorcraft Transmission Program
- Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
- Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
- Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation
- Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on parallel computers
- Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on parallel computers
- Aircraft of the future
- Alleviation of whirl-flutter on a joined-wing tilt-rotor aircraft configuration using active controls
- An efficient multiblock method for aerodynamic analysis and design on distributed memory systems : to be presented at the AIAA 13th Computational Fluid Dynamics Conference, June 1997
- An overview of the NASA F-18 high alpha research vehicle
- Analysis of NLR configurations using OCM for pilot modeling
- CFD analysis and design optimization using parallel computers
- Computations on wings with full-span oscillating control surfaces using Navier-Stokes equations
- Development of a computer program for analyzing preliminary aircraft configurations in relationship to emerging agility metrics : a thesis ...
- Dual-mission large aircraft feasibility study and aerodynamic investigation : research summary--year two, for contract NAG-1-1662
- Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
- Economic evaluation of flying-qualities design criteria for a transport configured with relaxed static stability
- Empennage noise shielding benefits for an open rotor transport
- Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature
- Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models
- Feasibility study for a microwave-powered ozone sniffer aircraft, Volume II
- Final report for the advanced concept studies for supersonic commercial transports entering service in the 2030 to 2035 period, N+3 Supersonic Program
- Fuselage design for a specified Mach-sliced area distribution
- High speed research system study : advanced flight deck configuration effects
- High-speed research : 1994 Sonic Boom Workshop : configuration design, analysis, and testing : proceedings of a workshop ... held in Hampton, Virginia, June 1-3, 1994
- Initial piloted simulation evaluation of the Reference-H High-Speed Civil Transport design during takeoff and recovery from limit flight conditions
- Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel
- Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration
- Low-speed wind tunnel tests of two waverider configuration models
- N+3 advanced concept studies for supersonic commercial transport aircraft entering service in the 2030-2035 period
- NASA Fixed Wing Project propulsion research and technology development activities to reduce thrust specific energy consumption
- NASA collaborative research on the ultra high bypass engine cycle and potential benefits for noise, performance, and emissions
- NASA/USRA high altitude reconnaissance aircraft, Volume 1
- Numerical study of steady and unsteady canard-wing-body aerodynamics
- Numerical study of three-dimensional separation and flow control at a wing-body junction : progress report for the period ended April 30, 1989
- Operational overview for UAS integration in the NAS project flight test series 3
- Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system
- Piloted simulation study of the effect of high-lift aerodynamics on the takeoff noise of a representative high-speed civil transport
- Prediction of forces and moments for flight vehicle control effectors
- Silent aircraft initiative concept risk assessment
- Study for prediction of rotor/wake/fuselage interference
- Supersonic flow computations for an ASTOVL aircraft configuration : phase 2, part 2
- TAS- a transonic aircraft/store flow field prediction code
- The effects of shot and laser peening on fatigue life and crack growth in 2024 aluminum alloy and 4340 steel
- Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling
- Utilization of an agility assessment module in analysis and optimization of preliminary fighter configuration
- V/STOL wind-tunnel testing
- Variable-complexity multidisciplinary optimization on parallel computers : final report, NAG-1-1562
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/FJV6ouGZJI4/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/FJV6ouGZJI4/">Aircraft configurations</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/FJV6ouGZJI4/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/FJV6ouGZJI4/">Aircraft configurations</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
