Download or read book Transonic Wind tunnel Investigation of the Effects of Incidence and Body Indentation on the Wing Loads of a 45 Degree Sweptback Wing body Combination written by Robert J. Jr Platt and published by . This book was released on 1956 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Effects of Wing Incidence on the Aerodynamic Loading Characteristics of a Sweptback Wing body Combination at Transonic Speeds written by Harold L. Robinson and published by . This book was released on 1954 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Transonic Wind tunnel Investigation of the Effects of Body Indentation as Specified by the Transonic Drag rise Rule on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degree Sweptback wing body Combination written by Harold L. Robinson and published by . This book was released on 1953 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Transonic Wind tunnel Investigation of the Effects of Twist and Camber with and Without Incidence Twist and Body Indentation on the Aerodynamic Characteristics of a 45 Degree Sweptback Wing body Configuration written by J. Lawrence Cooper and published by . This book was released on 1954 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Transonic Wind tunnel Investigation of the Effects of Body Indentation as Specified by the Transonic Drag rise Rule on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degrees Sweptback wing body Combination written by Harold L. Robinson and published by . This book was released on 1953 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Transonic Wind tunnel Investigation of the Effect of Modifications to an Indented Body in Combination with a 45 Degree Sweptback Wing written by Donald L. Loving and published by . This book was released on 1953 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Transonic Wind tunnel Investigation of the Effects of Taper Ratio Body Indentation Fixed Transition and Afterbody Shape on the Aerodynamic Characteristics of a 45 Degree Sweptback Wing body Combination written by Francis G. Morgan and published by . This book was released on 1954 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made to determine the effects of taper ratio, body indentation, fixed transition, and afterbody shape on the transonic aerodynamic characteristics of a 45 degree sweptback wing-body combination having an aspect ratio of 4. The results were obtained in the Langley 8-foot transonic tunnel at Mach numbers from 0.80 to 1.15, angles of attack from 0 to 12 degrees, and Reynolds numbers varying from 1,800,000 to 2,000,000 based on the mean aerodynamic chord of the wings.

Download or read book Transonic Wind tunnel Investigation of the Interference Between a 45 Sweptback Wing and a Systematic Series of Four Bodies written by Donald L. Loving and published by . This book was released on 1952 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Transonic Wind tunnel Investigation of Aerodynamic loading Characteristics of a 2 percent thick Trapezoidal Wing in Combination with Basic and Indented Bodies written by Thomas C. Kelly and published by . This book was released on 1957 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure data have been obtained in the Langley 8-foot transonic tunnel at Mach numbers from 0.80 to 1.115 and angles of attack from 0 to 20 degrees for wing-body configurations employing a thin trapezoidal wing in combination with basic and indented bodies. The wing had 26.6 degrees sweepback of the quarter-chord line, an aspect ratio of 2.61, a taper ratio of 0.211, and 2-percent-thick symmetrical circular-arc airfoil sections parallel to the plane of symmetry. Results are also presented for the basic body alone. Reynolds numbers for the tests were on the order of 2,600,000, based on the wing mean aerodynamic chord.

Download or read book Transonic Wind tunnel Investigation of the Effects of Aspect Ratio Spanwise Variations in Section Thickness Ratio and a Body Indentation on the Aerodynamic Characteristics of a 45 Degree Sweptback Wing body Combination written by Melvin M. Carmel and published by . This book was released on 1953 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Cost Utilization Analysis of Inhaled Steroids for Allergic Rhinitis Management written by and published by . This book was released on 2002 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1956 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Transonic Wind tunnel Investigation of the Effects of Taper Ratio and Body Indentation on the Aerodynamic Loading Characteristics of a 45 Sweptback Wing in the Presence of a Body written by James Benjamin Delano and published by . This book was released on 1955 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Transonic Wind tunnel Investigation of the Effects of Sweepback and Thickness Ratio on the Wing Loads of a Wing body Combination of Aspect Ratio 4 and Taper Ratio 0 6 written by Robert J. Platt and published by . This book was released on 1955 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: A transonic investigation of the effects of sweepback and thickness ratio on the wing loads of a wing in the presence of a body has been made in the Langley 8-foot transonic pressure tunnel. The tests covered wings with a thickness ratio of 6 percent for sweepback angles of 0, 25, and 45 degrees and a thickness ratio of 4 percent for an unswept wing.

Download or read book Wind tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0 1 to 0 8 on the Aerodynamic Characteristics in Pitch of the 45 Sweptback wing body Combination written by Harold S. Johnson and published by . This book was released on 1953 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Index of NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1959 with total page 500 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Transonic wind Tunnel Investigation of the Effects of Wing Incidence Angle on the Characteristics of Two Wing body Combinations written by Francis G. Jr Morgan and published by . This book was released on 1953 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: