Linearized Theory Of Wind Tunnel Jet Boundary Corrections And Ground Effect For Vtol Stol Aircraft
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Author |
: Harry H. Heyson |
Publisher |
: |
Total Pages |
: 286 |
Release |
: 1962 |
ISBN-10 |
: NASA:31769000421688 |
ISBN-13 |
: |
Rating |
: 4/5 (88 Downloads) |
Synopsis Linearized Theory of Wind-tunnel Jet-boundary Corrections and Ground Effect for Vtol-Stol Aircraft by : Harry H. Heyson
Interference factors are developed as a function of the degree to which the wake is deflected downward. At large wake deflections the interference may be much greater than indicated by classical theory. Methods are given for extending the present numerical results to tests involving multielement and finite-span models. The theory can be at least partially verified by means of available data. Tables of calculated interference factors are presented in NASA Technical Notes D-933, D-934, D-935, and D-936.
Author |
: Harry H. Heyson |
Publisher |
: |
Total Pages |
: 280 |
Release |
: 1962 |
ISBN-10 |
: UIUC:30112106738195 |
ISBN-13 |
: |
Rating |
: 4/5 (95 Downloads) |
Synopsis Linearized Theory of Wind-tunnel Jet-boundary Corrections and Ground Effect for Vtol-Stol Aircraft by : Harry H. Heyson
Author |
: Harry H. Heyson |
Publisher |
: |
Total Pages |
: 124 |
Release |
: 1969 |
ISBN-10 |
: UIUC:30112106738260 |
ISBN-13 |
: |
Rating |
: 4/5 (60 Downloads) |
Synopsis Use of Superposition in Digital Computers to Obtain Wind-tunnel Interference Factors for Arbitrary Configurations, with Particular Reference to V/STOL Models by : Harry H. Heyson
A superposition method utilizing a digital computer is developed to obtain wall interference for arbitrary configurations. A variety of specific configurations are treated. Sample numerical results indicate that a large number of variables, such as wind-tunnel configuration, model configuration, wake deflection, model location, span of wing and tail, load distribution, sweep, angle of attack, pivot location, tail length, and tail height, may individually or collectively produce substantial effects on wall interference. Interference is particularly severe at the rear rotor of tandem systems; the maximum size of such systems for reasonable wall effects is discussed.
Author |
: |
Publisher |
: |
Total Pages |
: 608 |
Release |
: 1976 |
ISBN-10 |
: MINN:31951000846563V |
ISBN-13 |
: |
Rating |
: 4/5 (3V Downloads) |
Synopsis NASA Technical Note by :
Author |
: E. M. Kraft |
Publisher |
: |
Total Pages |
: 74 |
Release |
: 1974 |
ISBN-10 |
: UOM:39015104953099 |
ISBN-13 |
: |
Rating |
: 4/5 (99 Downloads) |
Synopsis Analytical Study of Ventilated Wind Tunnel Boundary Interference on V/STOL Models Including Wake Curvature and Decay Effects by : E. M. Kraft
The wind tunnel boundary interference on a V/STOL model is calculated in a rectangular test section with solid vertical walls and ventilated (perforated or slotted) horizontal walls. The interference is found by applying the small perturbation theory of an incompressible fluid to the boundary value problem. The theory uses an image method in addition to Fourier transforms with an equivalent homogeneous boundary condition on the ventilated wall. The mathematical representation of the V/STOL model accounts for the curvature and decay of the wake. The assumption of a constant wake strength produces a paradox in that the maximum value of the interference factors increases as the initial jet velocity decreases. The most significant aspect of the analysis shows that nonlinear cross-flow effects at the tunnel boundary are important in the V/STOL case, and a quasi-linear approximation to these effects is introduced into the solution providing good agreement with experimental data.
Author |
: Matthew M. Winston |
Publisher |
: |
Total Pages |
: 84 |
Release |
: 1969 |
ISBN-10 |
: STANFORD:36105024772498 |
ISBN-13 |
: |
Rating |
: 4/5 (98 Downloads) |
Synopsis Wind-tunnel Data from a 0.16-scale V/STOL Model with Direct-lift and Lift-cruise Jets by : Matthew M. Winston
Author |
: |
Publisher |
: |
Total Pages |
: 1116 |
Release |
: 1962 |
ISBN-10 |
: UCAL:C2682417 |
ISBN-13 |
: |
Rating |
: 4/5 (17 Downloads) |
Synopsis Applied Mechanics Reviews by :
Author |
: Kenneth W. Goodson |
Publisher |
: |
Total Pages |
: 114 |
Release |
: 1967 |
ISBN-10 |
: UIUC:30112106688267 |
ISBN-13 |
: |
Rating |
: 4/5 (67 Downloads) |
Synopsis Effect of Ground Proximity on the Longitudinal, Lateral, and Control Aerodynamic Characteristics of a Tilt-wing Four-propeller V/STOL Model by : Kenneth W. Goodson
Author |
: |
Publisher |
: |
Total Pages |
: 688 |
Release |
: 1971 |
ISBN-10 |
: MINN:31951000846649L |
ISBN-13 |
: |
Rating |
: 4/5 (9L Downloads) |
Synopsis NASA Technical Report by :
Author |
: Kalman J. Grunwald |
Publisher |
: |
Total Pages |
: 84 |
Release |
: 1971 |
ISBN-10 |
: UIUC:30112106881649 |
ISBN-13 |
: |
Rating |
: 4/5 (49 Downloads) |
Synopsis Experimental Investigation of the Use of Slotted Test-section Walls to Reduce Wall Interference for High-lift-model Testing by : Kalman J. Grunwald