Download or read book Results of the TOBI 1 8 Scale Model Wind Tunnel Tests written by A. R. Packwood and published by . This book was released on 1984 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Advanced Recovery Systems Wind Tunnel Test Report written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pioneer Aerospace Corporation (PAC) conducted parafoil wind tunnel testing in the NASA-Ames 80 by 120 test sections of the National Full-Scale Aerodynamic Complex, Moffett Field, CA. The investigation was conducted to determine the aerodynamic characteristics of two scale ram air wings in support of air drop testing and full scale development of Advanced Recovery Systems for the Next Generation Space Transportation System. Two models were tested during this investigation. Both the primary test article, a 1/9 geometric scale model with wing area of 1200 square feet and secondary test article, a 1/36 geometric scale model with wing area of 300 square feet, had an aspect ratio of 3. The test results show that both models were statically stable about a model reference point at angles of attack from 2 to 10 degrees. The maximum lift-drag ratio varied between 2.9 and 2.4 for increasing wing loading. Geiger, R. H. and Wailes, W. K. Unspecified Center AERODYNAMICS; AIRDROPS; PARAFOILS; PARAFOILS; WIND TUNNEL TESTS; WINGS; ANGLE OF ATTACK; ASPECT RATIO; LIFT DRAG RATIO; SCALE MODELS; SPACE TRANSPORTATION SYSTEM; STABILITY; SUPPORT SYSTEMS...
Download or read book Wind Tunnel Tests on a 1 9 Scale Model of the Fairey Battle and a Comparison of the Results with Full scale Performance Data written by W. F. Campbell and published by . This book was released on 1943 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Tests on a 1 8th Scale Model of the Northrop Delta Landplane and Seaplane written by J. J. Green and published by . This book was released on 1937 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Test Results of a 1 written by John C. Wilson and published by . This book was released on 1996 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Test Techniques written by Colin Britcher and published by Academic Press. This book was released on 2023-10-20 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind Tunnel Test Techniques: Design and Use at Low and High Speeds with Statistical Engineering Applications provides an up-to-date treatment of the topic. Beginning with a brief history of wind tunnels and its types and uses, the book goes on to cover subsonic, supersonic and hypersonic wind tunnel design and construction, calibration, boundary corrections, flow quality assessment, pressure surveys, and dynamic testing. It also focuses on wind tunnel facilities, making it useful for both the designer and operator. Engineers and graduate students in aerospace, automotive and similar programs will find this book useful in their work with experimental aerodynamics, gas dynamics, facility design and performance. - Deals with a broad range of flow speeds in wind tunnels, from low speed to high speed - Provides a discussion of similarity laws as well as material on statistical analysis - Includes coverage on facility-to-facility and facility-to-CFD correlation - Presents advanced topics such as cryogenic wind tunnels, ground simulation in automotive testing, and propulsion testing
Download or read book Results of a Series of Wind Tunnel Tests on the BAC 1 11 Aircraft and a Comparison with Drag Estimates and Full scale Flight Data written by J. I. Simper and published by . This book was released on 1972 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Tests of the 1 8 scale Powered Model of the Curtiss XBTC 2 Airplane written by Joseph Weil and published by . This book was released on 1944 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: A series of wind-tunnel tests was made in the LMAL 7- by 10-foot tunnel of the Curtiss XBTC-2 model (1/8-scale) with power to determine and improve, as necessary, the complete aerodynamic characteristics of the model.
Download or read book Wind Tunnel Tests on a 1 8 Scale Model Northrop Delta Aircraft with Armament Equipment written by J. J. Green and published by . This book was released on 1938 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Large scale V STOL Testing written by and published by . This book was released on 1977 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Tests of a 0 06 scale B 1 Model at Mach Numbers from 0 60 to 1 60 written by C. J. Spurlin and published by . This book was released on 1973 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Data from a 0 16 scale V STOL Model with Direct lift and Lift cruise Jets written by Matthew M. Winston and published by . This book was released on 1969 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Effect of Compressibility on a 11 scale Model of the A 20 Attack Bomber from Tests in the N A C A 8 foot High speed Wind Tunnel written by James B. Delano and published by . This book was released on 1944 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Design of a Laminar Flow Low Turbulence Wind Tunnel and Results of Tests Conducted with a Half Scale Model written by Eugene Harris Handler and published by . This book was released on 1949 with total page 224 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive cylinder Model at Mach Numbers 1 75 to 4 50 written by Neil Arthur Zarin and published by . This book was released on 1964 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Full scale 1903 Wright Flyer Wind Tunnel Test Results from the NASA Ames Research Center written by Henry R. Jex and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Study of the Integration of Wind Tunnel and Computational Methods for Aerodynamic Configurations written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11-12 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was conducted to determine the effectiveness of using a low-order panel code to estimate wind tunnel wall corrections. The corrections were found by two computations. The first computation included the test model and the surrounding wind tunnel walls, while in the second computation the wind tunnel walls were removed. The difference between the force and moment coefficients obtained by comparing these two cases allowed the determination of the wall corrections. The technique was verified by matching the test-section, wall-pressure signature from a wind tunnel test with the signature predicted by the panel code. To prove the viability of the technique, two cases were considered. The first was a two-dimensional high-lift wing with a flap that was tested in the 7- by 10-foot wind tunnel at NASA Ames Research Center. The second was a 1/32-scale model of the F/A-18 aircraft which was tested in the low-speed wind tunnel at San Diego State University. The panel code used was PMARC (Panel Method Ames Research Center). Results of this study indicate that the proposed wind tunnel wall correction method is comparable to other methods and that it also inherently includes the corrections due to model blockage and wing lift. Browne, Lindsey E. and Ashby, Dale L. Ames Research Center...
