Download or read book Comparison of Large scale Flight Measurements of Zero lift Drag at Mach Numbers from 0 9 to 1 7 of Two Wing body Combinations Having Similar 60 Degree Triangular Wings with NACA 65A003 Sections written by Eugene D. Schult and published by . This book was released on 1950 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Comparison of Large scale Flight Measurements of Zero lift Drag at Mach Numbers from 0 9 to 1 7 of Two Wing body Combinations Having Similar 60 Degrees Triangular Wings with NACA 65A003 Sections written by Eugene D. Schult and published by . This book was released on 1951 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Large scale Flight Measurements of Zero lift Drag at Mach Numbers from 0 86 to 1 5 of a Wing body Combination Having a 60 Degree Triangular Wing with NACA 65A003 Sections written by Robert L. Nelson and published by . This book was released on 1950 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Large scale Flight Measurements of Zero lift Drag and Low lift Drag of 10 Wing body Configurations at Mach Numbers from 0 8 to 1 6 written by John D. Morrow and published by . This book was released on 1953 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Large scale Flight Measurements of Zero lift Drag at Mach Numbers from 0 86 to 1 5 of a Wing body Combination Having a 60 Degrees Triangular Wing with NACA 65A003 Sections written by Robert L. Nelson and published by . This book was released on 1951 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Free flight Measurements of the Zero lift Drag of Several Wings at Mach Numbers from 1 4 to 3 8 written by H. Herbert Jackson and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Large scale Flight Measurements of Zero lift Drag at Mach Numbers from 0 8 to 1 6 of a Wing body Combination Having an Unswept 4 5 percent thick Wing with Modified Hexagonal Sections written by Eugene D. Schult and published by . This book was released on 1951 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Large Scale Flight Measurements of Zero lift Drag and Low lift Longitudinal Characteristics of a Diamond wing body Combination at Mach Numbers from 0 725 to 1 54 written by Harvey A. Wallskog and published by . This book was released on 1953 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2 0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Large scale Flight Measurements of Zero lift Drag and Low lift Drag Longitudinal Characteristics of a Diamond wing body Combination at Mach Numbers from 0 725 to 1 54 written by Harvey A. Wallskog and published by . This book was released on 1953 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Large scale Flight Measurements of Zero lift Drag at Mach Numbers from 0 90 to 1 95 of an Arrow Wing in Combination with a Small Body written by Warren Jr Gillespie and published by . This book was released on 1951 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Large scale Flight Measurements of Zero lift Drag of 10 Wing body Configurations at Mach Numbers from 0 8 to 1 6 written by John D. Morrow and published by . This book was released on 1953 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Drag Due to Lift at Mach Numbers Up to 2 0 written by Edward C. Polhamus and published by . This book was released on 1953 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Results of a Flight Investigation to Determine the Zero Lift Drag Characteristics of a 60 Deg Delta Wing with NACA 65 006 Airfoil Section and Various Double Wedge Sections at Mach Numbers from 0 7 1 6 written by and published by . This book was released on 1956 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of an exploratory free-flight investigation at zero lift of several rocket-powered drag-research models equipped with 60 deg sweptback delta wings are presented for a Mach number range from about 0.70 to 1.60. The airfoil sections tested included the NACA 65-006 and a series of double-wedge sections with various thicknesses and positions of maximum thickness. The results of the investigation showed that, of the double-wedge sections with 6 percent thickness, the two sections with positions of maximum thickness at 20 and 50 percent of the chord had drag coefficients approximately equal through the transonic and supersonic Mach number range and had similarly occurring drag rises. The section with position of maximum thickness at 80 percent chord had a drag rise occurring at a Mach number M of approximately 0.15 lower than the drag rise of the other two sections. At M = 1.0, this section had drag coefficients more than twice as large as those of the other two sections; however, this difference decreased with increasing supersonic Mach numbers. The wing drag calculated by the linearized theory was in qualitative agreement with the test results in indicating the effects of varying the position of maximum thickness. The double-wedge section of 5 percent thickness with position of maximum thickness at 50 percent chord had fairly constant drag coefficients throughout the supersonic region, which ranged from about 50 to 80 percent of the drag coefficients for the similar section with twice the thickness ratio. The theoretical wing drag for this section was in very good agreement with the experimental value. The NACA 65-006 airfoil section had lower drag coefficients throughout the test region than any of the double-wedge sections of the same thickness ratio, although at the highest Mach numbers covered by these tests, the differences became very small.

Download or read book Measured and Predicted Section Wave Drag Coefficients at a Mach Number of 1 6 for a Delta Wing with Two Airfoil Sections written by Frederick C. Grant and published by . This book was released on 1959 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental Pressure Distributions Over Two Wing body Combinations at Mach Number 1 9 written by Barry Moskowitz and published by . This book was released on 1951 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: Pressure distributions on two wing-body combinations were obtained at Mach number of 1.9 to investigate wing-body interference. A rectangular wing, a triangular wing, and a cylindrical body having an ogive nose were investigated alone and in combination. Pressure distributions over the wing body combination compared favorable with theoretical calculations based primarily on a generalization of the method of Nielsen and Matteson, except at the root section of wings where boundary layer of body modified the flow.

Download or read book Influence of the Body Flow Field on the Zero lift Wave Drag of Wing body Combinations Modified in Accordance with the Transonic Area Rule written by William A. Page and published by . This book was released on 1956 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: