Aerodynamic load
Resource Information
The concept Aerodynamic load represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
The Resource
Aerodynamic load
Resource Information
The concept Aerodynamic load represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
- Label
- Aerodynamic load
- Authority link
- (EG-IN)1251803
40 Items that share the Concept Aerodynamic load
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- Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
- A characteristic method for calculating the generalized flat flutter aerodynamic forces
- A modification to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack
- A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
- A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft
- Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations
- Aerodynamic forces on freight trains
- Airloads on bluff bodies, with application to the rotor-induced downloads on tilt-rotor aircraft
- An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades
- An experimental and theoretical analysis of the aerodynamic characteristics of a biplane-winglet configuration
- An experimental study of fluctuating pressure loads beneath swept shock/boundary layer interactions
- Analysis and compilation of missile aerodynamic data
- Combined experiment : final report, Phase I
- Comparison of concurrent strain gage- and pressure transducer-measured flight loads on a lifting reentry vehicle and correlation with wind tunnel predictions
- Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
- Correlation of forebody pressures and aircraft yawing moments on the X-29A aircraft at high angles of attack
- Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output
- Development of an unsteady aerodynamic analysis for finite-deflection subsonic cascades
- Development of the triplet singularity for the analysis of wings and bodies in supersonic flow
- Early operation experience on the ERDA/NASA 100 kW wind turbine
- Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing
- Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
- Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9
- Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
- Experimental investigation of effects of blade tip geometry on loads and performance for an articulated rotor system
- Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
- F-18 High Alpha Research Vehicle surface pressures : initial in-flight results and correlation with flow visualization and wind-tunnel data
- F-8 supercritical wing flight pressure, boundary-layer, and wake measurements and comparisons with wind tunnel data
- Fluctuating loads measured on an over-the-wing supersonic jet model
- Loads and motions of an F-106B flying through thunderstorms
- Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds
- Nacelle Aerodynamic and Inertial Loads (NAIL) project : summary report, Oct. 1979 - Aug. 1981
- Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20
- Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel
- Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel
- Some properties of a five-parameter bivariate probability distribution
- Studies of air loads on man
- The measurement and assessment of repeated loads on airplane components : presented to the 3rd meeting of the Structures and Material Panel of AGARD, Langley Field, Virginia, April 12, 1956
- Theoretical and experimental study of twisted and cambered delta wings designed for a Mach number of 3.5
- Thermal stress analysis of ceramic gas-path seal components for aircraft turbines
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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.library.in.gov/resource/FeyurtIA60Q/" 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/FeyurtIA60Q/">Aerodynamic load</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>
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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.library.in.gov/resource/FeyurtIA60Q/" 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/FeyurtIA60Q/">Aerodynamic load</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>
