Aerodynamic Characteristics at Transonic Speeds of an Airplane Configuration with an 83.5 Deg Delta Wing Having Auxiliary Variable-sweep Wing Panels
Author:
Publisher:
Published: 1963
Total Pages: 230
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author:
Publisher:
Published: 1963
Total Pages: 230
ISBN-13:
DOWNLOAD EBOOKAuthor: Arvo A. Luoma
Publisher:
Published: 1961
Total Pages: 88
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1961
Total Pages: 86
ISBN-13:
DOWNLOAD EBOOKAuthor: Ralph P. Bielat
Publisher:
Published: 1960
Total Pages: 84
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1963
Total Pages: 70
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1963
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1963
Total Pages: 52
ISBN-13:
DOWNLOAD EBOOKAuthor: M. Leroy Spearman
Publisher:
Published: 1961
Total Pages: 36
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1960
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKAuthor: William C. Sleeman
Publisher:
Published: 1949
Total Pages: 34
ISBN-13:
DOWNLOAD EBOOKThis paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.