Download or read book Longitudinal Stability Control Effectiveness and Drag Characteristics at Transonic Speeds of a Rocket propelled Model of an Airplane Configuration Having an Unswept Tapered Wing of Aspect Ratio 3 0 and NACA 65A004 5 Airfoil Sections written by John C. Jr McFall and published by . This book was released on 1953 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability Characteristics at Transonic Speeds of a Rocket propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6 0 written by John C. McFall and published by . This book was released on 1954 with total page 44 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 Longitudinal Stability Characteristics at Transonic Speeds of a Rocket propelled Model of an Airplane Configuration Having a 45 Degree Swept Wing of Aspect Ratio 6 0 written by John C. Jr McFall and published by . This book was released on 1954 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability and Drag Characteristics at Mach Numbers from 0 75 to 1 5 of an Airplane Configuration Having a 60 Degrees Swept Wing of Aspect Ratio 2 24 as Obtained from Rocket propelled Model written by A. James Vitale and published by . This book was released on 1952 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability and Control Characteristics at High Subsonic Speeds of Two Models of a Transonic Research Airplane with Wings and Horizontal Tails of Aspect Ratios 4 2 and 2 written by Arvo A. Luoma and published by . This book was released on 1950 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley 8-foot high-speed tunnel of two transonic research airplane models for Mach numbers up to approximately 0.95. The test Reynolds number at the highest speed was 1,600,000 for one model and 2,300,000 for the other model. The models were 1/16-schale and were supported in the tunnel on a sting. The wing and horizontal tail of one model were both of aspect ratio 4.2; the wing and horizontal tail of the other model were both of aspect ratio 2. The same fuselage and vertical tail were used on both models. The sweep of the 50-percent-chord line of the wings was zero degrees; the sweep of the 75-percent-chord line of the horizontal tails was zero degrees. Both wings had NACA 65-110 airfoil sections and both horizontal tails had NACA 65-008 airfoil sections. Lift drag, and pitching moment were determined by means of a strain-gage balance within the fuselage. Tare measurements were made to eliminate the interference effect of the sting.

Download or read book Longitudinal Stability Trim and Drag Characteristics of a Rocket propelled Model of an Airplane Configuration Having a 45 Degree Sweptback Wing and an Unswept Horizontal Tail written by James H. Parks and published by . This book was released on 1952 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability and Control Characteristics of a Semispan Airplane Model with a Swept back Tail from Tests at Transonic Speeds by the NACA Wing flow Method written by John A. Zalovcik and published by . This book was released on 1947 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made by the NACA wing-flow method to determine the longitudinal stability and control characteristics at transonic speeds of a semispan airplane model having a wing of conventional plan form and a horizontal tail swept back 45 degrees. The wing and tail had NACA 65-series airfoil sections with thicknesses of 10 and 8 percent chord, respectively. The model was mounted in such a way as to permit it to assume a position of zero pitching moment about a center of gravity at 27 percent of the mean aerodynamic chord. Measurements were made of lift and angle of attack for trim for several stabilizer and elevator settings.

Download or read book Stability and Control Characteristics at Transonic Speeds of Two Variable sweep Airplane Configurations Differing in Wing pivot Locations written by Ralph P. Bielat and published by . This book was released on 1961 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Miscellaneous Directional stability Data for Several Airplane like Configurations from Rocket model Tests at Transonic Speeds written by Paul E. Purser and published by . This book was released on 1952 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like configurations flown as rocket models for other purposes, at transonic speeds, have been collected and compared with the available subsonic and supersonic wind-tunnel data for the same configurations.

Download or read book Longitudinal Stability and Control Characteristics at Transonic Speeds of a Semispan Airplane Model Having a 45 Degrees Sweptback Wing and Tail as Obtained by the Transonic bump Method written by M. Leroy Spearman and published by . This book was released on 1948 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability and Control Characteristics of a Semispan Airplane Model at Transonic Speeds from Tests by the NACA Wing flow Method written by John A. Zalovcik and published by . This book was released on 1946 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Determination of Longitudinal Stability and Control Characteristics from Free flight Model Tests with Results at Transonic Speeds for Three Airplane Configurations written by Clarence L. Gillis and published by . This book was released on 1957 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability and Control Characteristics of an Airplane Model Having a 42 8 Deg Sweptback Circular Arc Wing with Aspect Ratio 4 00 Taper Ratio 0 50 and Sweptback Tail Surfaces written by and published by . This book was released on 1947 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability and Control Characteristics of a Semispan Airplane Model with a Sweptback Wing and Tail from Tests at Transonic Speeds by the NACA Wing flow Method written by Richard H. Sawyer and published by . This book was released on 1948 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Comparison of Low lift Drag at Mach Numbers from 0 74 to 1 37 of Rocket boosted Models Having Externally Braced Wings and Cantilever Wings written by Waldo L. Dickens and published by . This book was released on 1957 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted to determine whether the low-lift drag of a rocket-model airplane-like configuration could be reduced at transonic and low supersonic Mach numbers by reducing the wing thickness while external braces were used to provide the necessary bending strength. The investigation consisted of flight training two rocket models having aspect ratio 3.04, unswept braced tapered wings mounted on fuselages with the same fineness ratios and cross-sectional area distributions. Data collected from the flight test of a model having a thicker cantilever wing of the same plan form were compared with data collected in this investigation.

Download or read book Analytical Study of the Effect of Center of gravity Position on the Response to Longitudinal Control in Landing Approaches of a Swept wing Airplane of Low Aspect Ratio Having No Horizontal Tail written by Ralph W. Stone and published by . This book was released on 1954 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical study of the short-time response characteristics to longitudinal control moments of a swept-wing airplane of low aspect ratio having no horizontal tail has indicated that difficulty reported in landings aboard an aircraft carrier may have been the result of a relatively larger time lag in the response of the airplane in changing its flight-path angle than exists on more conventional type airplanes. It has been reasoned that reduction of the airplane's static longitudinal stability might improve the response characteristics. Accordingly, an analytical study of the effect of reducing the static stability by a practical center-of-gravity shift has been made.