Investigation At Transonic Speeds Of The Loading Over A 45 Degree Sweptback Wing Having An Aspect Ratio Of 3 A Taper Ratio Of 0 2 And Naca 65a004 Airfoil Sections
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Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3 a Taper Ratio of 0 2 and NACA 65A004 Airfoil Sections
Author | : Jack F. Runckel |
Publsiher | : Unknown |
Total Pages | : 104 |
Release | : 1956 |
Genre | : Aerodynamic load |
ISBN | : UOM:39015095100999 |
Download Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3 a Taper Ratio of 0 2 and NACA 65A004 Airfoil Sections Book in PDF, Epub and Kindle
An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections has been conducted in the Langley16-foot transonic tunnel. Pressure measurements on the wing-body combination were obtained at angles of attack from 0 to 26 degrees at Mach numbers from 0.80 to 0.98 and from 0 to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic chord, varied from 7,000,000 to 8,500,000 over the test Mach number range.
Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3 a Taper Ratio of 0 2 and Naca 65a004 Airfoil Sections
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Author | : JACK F. RUNCKEL,EDWIN E. JR. LEE,NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C. |
Publsiher | : Unknown |
Total Pages | : 1 |
Release | : 1961 |
Genre | : Electronic Book |
ISBN | : OCLC:227261890 |
Download Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3 a Taper Ratio of 0 2 and Naca 65a004 Airfoil Sections Book in PDF, Epub and Kindle
An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections was conducted in the Langley 16-foot transonic tunnel. Pressure measurements on the wing-body combi ation were obtained at angles of attack from 0 degrees to 26 degrees at Mach numbers from 0.80 to 0.98 and at angles of attack from 0 degrees to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic c ord varied from 7 times 10 to the 6th po er to 8.5 times 10 to the 6th power over the test Mach number range. Results of the investigation indicate that a highly swept shock originates at the juncture of the wing leading edge and the body at moderate angles of attack and has a large influence on the loading over the inboard wing sections. (Author).
Investigation at Transonic Speeds of Loading Over a 30 Deg Sweptback Wing of Aspect Ratio 3 Taper Ratio 0 2 and NACA 65A004 Airfoil Section Mounted on a Body
Author | : Donald D. Arabian |
Publsiher | : Unknown |
Total Pages | : 88 |
Release | : 1960 |
Genre | : Aerodynamics, Transonic |
ISBN | : NASA:31769000456270 |
Download Investigation at Transonic Speeds of Loading Over a 30 Deg Sweptback Wing of Aspect Ratio 3 Taper Ratio 0 2 and NACA 65A004 Airfoil Section Mounted on a Body Book in PDF, Epub and Kindle
The aerodynamic load characteristics of a wing-body combination were determined experimentally at Mach numbers from 0.80 to 1.03 for angles of attack up to 26 degrees. Two wings, both with 30 degrees sweep of the quarter-chord line, taper ratio of 0.2, aspect ratio of 3, and thickness of 4 percent chord, but of different types of construction, were tested. One wing was of solid steel and the other was of plastic with an inner steel core ...
U S Government Research Reports
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 232 |
Release | : 1961 |
Genre | : Science |
ISBN | : UOM:39015086571661 |
Download U S Government Research Reports Book in PDF, Epub and Kindle
Investigation at Transonic Speeds of the Loading Over a 40 Degree Sweptback Wing Having an Aspect Ratio of 3 a Taper Ratio of 0 2 and NACA 65A004 Airfoil Sections
Author | : Jack F. Runckel |
Publsiher | : Unknown |
Total Pages | : 98 |
Release | : 1961 |
Genre | : Aerodynamics |
ISBN | : UIUC:30112106682393 |
Download Investigation at Transonic Speeds of the Loading Over a 40 Degree Sweptback Wing Having an Aspect Ratio of 3 a Taper Ratio of 0 2 and NACA 65A004 Airfoil Sections Book in PDF, Epub and Kindle
Index to NASA Technical Publications
Author | : United States. National Aeronautics and Space Administration |
Publsiher | : Unknown |
Total Pages | : 135 |
Release | : 1960-07 |
Genre | : Electronic Book |
ISBN | : STANFORD:36105024165701 |
Download Index to NASA Technical Publications Book in PDF, Epub and Kindle
An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4 percent thick 30 Degree Swepptback Wing at Transonic Speeds
Author | : Charles F. Whitcomb,Philippa F. Brown,Chris C. Critzos |
Publsiher | : Unknown |
Total Pages | : 286 |
Release | : 1961 |
Genre | : Electronic Book |
ISBN | : UIUC:30112106774372 |
Download An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4 percent thick 30 Degree Swepptback Wing at Transonic Speeds Book in PDF, Epub and Kindle
A Selected Listing of NASA Scientific and Technical Reports for
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 388 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : UVA:X004173287 |
Download A Selected Listing of NASA Scientific and Technical Reports for Book in PDF, Epub and Kindle