Analysis Of Pressure Data Obtained At Transonic Speeds On A Thin Low Aspect Ratio Cambered Delta Wing Body Combination PDF Download
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Author | : John P. Mugler |
Publisher | : |
Total Pages | : 126 |
Release | : 1958 |
Genre | : Transonic planes |
ISBN | : |
Download Analysis of Pressure Data Obtained at Transonic Speeds on a Thin Low-aspect-ratio Cambered Delta Wing-body Combination Book in PDF, ePub and Kindle
Author | : Earl R. Keener |
Publisher | : |
Total Pages | : 80 |
Release | : 1959 |
Genre | : Aerodynamic load |
ISBN | : |
Download Pressure Measurements Obtained in Flight at Transonic Speeds for a Conically Cambered Delta Wing Book in PDF, ePub and Kindle
Author | : John P. Mugler |
Publisher | : |
Total Pages | : 79 |
Release | : 1957 |
Genre | : Aerodynamic load |
ISBN | : |
Download Pressure Measurements at Transonic and Low Supersonic Speeds on a Thin Conical Cambered Low-aspect-ratio Delta Wing in Combination with Basic and Indented Bodies Book in PDF, ePub and Kindle
Pressure distributions on a thin conical cambered low-aspect-ratio delta wing have been obtained in the Langley 8-foot transonic tunnel over a Mach number range from 0.60 to 1.12 and at a Mach number of 1.43. Data were obtained for the wing in combination with a basic Sears-Haack body and a body indented symmetrically for a Mach number of 1.2. The angle-of-attack range was from -4 to 20 degrees in most instances.
Author | : Earl R. Keener |
Publisher | : |
Total Pages | : 76 |
Release | : 1959 |
Genre | : |
ISBN | : |
Download Professional Measurements Obtained in Flight at Transonic Speeds for a Conically Cambered Delta Wing Book in PDF, ePub and Kindle
Author | : Marlowe D. Cassetti |
Publisher | : |
Total Pages | : 104 |
Release | : 1961 |
Genre | : Transonic wind tunnels |
ISBN | : |
Download Transonic Aerodynamic Loading Characteristics of a Wing-body-tail Combination Having 52.5° Sweptback Wing of Aspect Ratio 3 with Conical Wing Camber and Body Indentation for a Design Mach Number [square Root Of] 2 Book in PDF, ePub and Kindle
An investigation has been made of the effects of conical wing camber and body indentation according to the supersonic area rule on the aerodynamic wing loading characteristics of a wing-body-tail configuration at transonic speeds. The wing aspect ratio was 3, taper ratio was 0.1, and quarter-chord-line sweepback was 52.5° with 3-percent-thick airfoil sections. The tests were conducted in the Langley 16-foot transonic tunnel at Mach numbers from 0.80 to 1.05 and at angles of attack from 0° to 14°, with Reynolds numbers based on mean aerodynamic chord varying from 7 x 106 to 8 x 106. Conical camber delayed wing-tip stall and reduced the severity of the accompanying longitudinal instability but did not appreciably affect the spanwise load distribution at angles of attack below tip stall. Body indentation reduced to transonic chordwise center-of-pressure travel from about 8 percent to 5 percent of the mean aerodynamic chord.
Author | : |
Publisher | : |
Total Pages | : 442 |
Release | : 1961 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, ePub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 448 |
Release | : 1960 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NASA Technical Publications Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 818 |
Release | : 1954 |
Genre | : Aeronautics |
ISBN | : |
Download A Selected Listing of NASA Scientific and Technical Reports for ... Book in PDF, ePub and Kindle
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : |
Release | : 1960-07 |
Genre | : |
ISBN | : |
Download Index to NASA Technical Publications Book in PDF, ePub and Kindle
Author | : Defense Documentation Center (U.S.) |
Publisher | : |
Total Pages | : 1746 |
Release | : 1961-04 |
Genre | : Military art and science |
ISBN | : |
Download Technical Abstract Bulletin Book in PDF, ePub and Kindle