Wind Tunnel Wall Interference In V Stol And High Lift Testing
Download Wind Tunnel Wall Interference In V Stol And High Lift Testing full books in PDF, epub, and Kindle. Read online free Wind Tunnel Wall Interference In V Stol And High Lift Testing ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads.
Author |
: Marie H. Tuttle |
Publisher |
: |
Total Pages |
: 58 |
Release |
: 1986 |
ISBN-10 |
: STANFORD:36105024733763 |
ISBN-13 |
: |
Rating |
: 4/5 (63 Downloads) |
Synopsis Wind Tunnel Wall Interference in V/STOL and High Lift Testing by : Marie H. Tuttle
Author |
: Marie H. Tuttle |
Publisher |
: |
Total Pages |
: 60 |
Release |
: 1986 |
ISBN-10 |
: NASA:31769000576317 |
ISBN-13 |
: |
Rating |
: 4/5 (17 Downloads) |
Synopsis Wind Tunnel Wall Interference in V/STOL and High Lift Testing: A Selected, Annotated Bibliography by : Marie H. Tuttle
Author |
: |
Publisher |
: |
Total Pages |
: 64 |
Release |
: 1986 |
ISBN-10 |
: MINN:31951P00218741D |
ISBN-13 |
: |
Rating |
: 4/5 (1D Downloads) |
Synopsis NASA Technical Memorandum by :
Author |
: Marie H. Tuttle |
Publisher |
: |
Total Pages |
: 96 |
Release |
: 1988 |
ISBN-10 |
: UIUC:30112106721589 |
ISBN-13 |
: |
Rating |
: 4/5 (89 Downloads) |
Synopsis Wind Tunnel Wall Interference (January 1980-May 1988) by : Marie H. Tuttle
Author |
: T. W. Binion (Jr.) |
Publisher |
: |
Total Pages |
: 38 |
Release |
: 1975 |
ISBN-10 |
: UOM:39015104958601 |
ISBN-13 |
: |
Rating |
: 4/5 (01 Downloads) |
Synopsis An Experimental Study of Several Wind Tunnel Wall Configurations Using Two V/STOL Model Configurations by : T. W. Binion (Jr.)
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 |
: |
Publisher |
: |
Total Pages |
: 564 |
Release |
: 1973 |
ISBN-10 |
: MINN:31951000846483T |
ISBN-13 |
: |
Rating |
: 4/5 (3T Downloads) |
Synopsis NASA Technical Note by :
Author |
: |
Publisher |
: |
Total Pages |
: 712 |
Release |
: 1988 |
ISBN-10 |
: UOM:39015034725161 |
ISBN-13 |
: |
Rating |
: 4/5 (61 Downloads) |
Synopsis Scientific and Technical Aerospace Reports by :
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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 |
: |
Publisher |
: |
Total Pages |
: 946 |
Release |
: 1968 |
ISBN-10 |
: MINN:31951000846637S |
ISBN-13 |
: |
Rating |
: 4/5 (7S Downloads) |
Synopsis NASA Technical Report by :