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Wind Tunnel Investigation Of The Effects Of Steady Rolling On The Aerodynamic Loading Characteristics Of A 45c Sweptback Wing At High Subsonic Speeds
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Book Synopsis Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45 Degree Sweptback Wing at High Subsonic Speeds by : James W. Wiggins
Download or read book Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45 Degree Sweptback Wing at High Subsonic Speeds written by James W. Wiggins and published by . This book was released on 1953 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at High Subsonic Speeds of the Effects of Wing-mounted External Stores on the Loading and Aerodynamic Characteristics in Pitch of a 45 Degree Sweptback Wing Combined with a Fuselage by : H. Norman Silvers
Download or read book Wind-tunnel Investigation at High Subsonic Speeds of the Effects of Wing-mounted External Stores on the Loading and Aerodynamic Characteristics in Pitch of a 45 Degree Sweptback Wing Combined with a Fuselage written by H. Norman Silvers and published by . This book was released on 1954 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds by : James W. Wiggins
Download or read book Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds written by James W. Wiggins and published by . This book was released on 1956 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the horizontal- and vertical-tail contributions to the static lateral stability of a complete-model swept-wing configuration at high subsonic speeds. The results indicate that, in a general, Mach number effects within the range studied and wing effects on the tail contribution were small and the overall trends of the data of the present investigation agreed with those which have been established at low speeds.
Book Synopsis Wind-tunnel Investigation to Determine the Aerodynamic Characteristics in Steady Roll of a Model at High Subsonic Speeds by : Richard E. Kuhn
Download or read book Wind-tunnel Investigation to Determine the Aerodynamic Characteristics in Steady Roll of a Model at High Subsonic Speeds written by Richard E. Kuhn and published by . This book was released on 1953 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds by : Edward C. Polhamus
Download or read book The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds written by Edward C. Polhamus and published by . This book was released on 1955 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt: A summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip characteristics of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.
Book Synopsis Wind-tunnel Investigation at Subsonic and Low Transonic Speeds of the Effects of Aileron Span and Spanwise Location on the Rolling Characteristics of a Test Vehicle with Three Untapered 45 Degrees Sweptback Wings by : Harold S. Johnson
Download or read book Wind-tunnel Investigation at Subsonic and Low Transonic Speeds of the Effects of Aileron Span and Spanwise Location on the Rolling Characteristics of a Test Vehicle with Three Untapered 45 Degrees Sweptback Wings written by Harold S. Johnson and published by . This book was released on 1951 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation of the Interaction and Breakdown Characteristics of Slender-wing Vortices at Subsonic, Transonic, and Supersonic Speeds by : Gary E. Erickson
Download or read book Wind Tunnel Investigation of the Interaction and Breakdown Characteristics of Slender-wing Vortices at Subsonic, Transonic, and Supersonic Speeds written by Gary E. Erickson and published by . This book was released on 1991 with total page 230 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing-fuselage Combination with Quarter-chord Line Swept Back 32.6 Degrees and NACA 65A006 Airfoil Section by : Harold S. Johnson
Download or read book Wind-tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing-fuselage Combination with Quarter-chord Line Swept Back 32.6 Degrees and NACA 65A006 Airfoil Section written by Harold S. Johnson and published by . This book was released on 1953 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at High Subsonic Speeds of the Stability Characteristics of a Complete Model Having Sweptback-,M-,W-,and Cranked-wing Plan Forms and Several Horizontal-tail Locations by : Kenneth W. Goodson
Download or read book Wind-tunnel Investigation at High Subsonic Speeds of the Stability Characteristics of a Complete Model Having Sweptback-,M-,W-,and Cranked-wing Plan Forms and Several Horizontal-tail Locations written by Kenneth W. Goodson and published by . This book was released on 1954 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made at high subsonic speeds of a complete model having a basic sweptback wing or one of three composite plan-form wings. The composite plan-form wings (M, W, and cranked) were obtained through modifications to the basic 45 degree swept-wing design. All wings were of aspect ratio 4.0 and taper ratio 0.3. These wings were tested through an angle of attack range in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.80 to 0.92.
Book Synopsis 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 by : James Benjamin Delano
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:
Book Synopsis Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls by : Robert E. Dannenberg
Download or read book Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls written by Robert E. Dannenberg and published by . This book was released on 1950 with total page 678 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tunnel-wall corrections for the induced upwash velocity for a swept wing completely spanning a rectangular wind tunnel are included in the appendix.
Book Synopsis 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 a 45 Degree Sweptback-wing-body Combination by : Harold S. Johnson
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 a 45 Degree Sweptback-wing-body Combination written by Harold S. Johnson and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Studies of the Effects of Stimulated Damage on the Aerodynamic Characteristics of Airplanes and Missiles by :
Download or read book Wind-tunnel Studies of the Effects of Stimulated Damage on the Aerodynamic Characteristics of Airplanes and Missiles written by and published by . This book was released on 1982 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
