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Book Static Longitudinal Stability and Control Characteristics at Mach Numbers of 2 86 and 6 02 and Angles of Attack Up to 95 Deg of a Lenticular shaped Reentry Vehicle

Download or read book Static Longitudinal Stability and Control Characteristics at Mach Numbers of 2 86 and 6 02 and Angles of Attack Up to 95 Deg of a Lenticular shaped Reentry Vehicle written by and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal Stability and Control Characteristics at a Mach Number of 1 99 of a Lenticular shaped Reentry Vehicle

Download or read book Static Longitudinal Stability and Control Characteristics at a Mach Number of 1 99 of a Lenticular shaped Reentry Vehicle written by Charlie M. Jackson and published by . This book was released on 1960 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal and Lateral Stability Characteristics at a Mach Number of 3 11 of Square and Circular Plan form Reentry Vehicles  with Some Effects of Controls and Leading edge Extensions

Download or read book Static Longitudinal and Lateral Stability Characteristics at a Mach Number of 3 11 of Square and Circular Plan form Reentry Vehicles with Some Effects of Controls and Leading edge Extensions written by Byron M. Jaquet and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Low subsonic speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry vehicle Configuration Having Wingtip Panels that Fold Up for High drag Reentry

Download or read book Low subsonic speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry vehicle Configuration Having Wingtip Panels that Fold Up for High drag Reentry written by George M. Ware and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Longitudinal Stability and Control Characteristics of a Two place All weather Fighter Airplane Between Mach Numbers of 0 80 and 2 00 Obtained from the Flight Test of a Rocket boosted Model

Download or read book Longitudinal Stability and Control Characteristics of a Two place All weather Fighter Airplane Between Mach Numbers of 0 80 and 2 00 Obtained from the Flight Test of a Rocket boosted Model written by and published by . This book was released on 1959 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal  Directional  and Lateral Stability and Control Data at a Mach Number of 6 83 of the Final Configuration of the X 15 Research Airplane

Download or read book Static Longitudinal Directional and Lateral Stability and Control Data at a Mach Number of 6 83 of the Final Configuration of the X 15 Research Airplane written by Jim A. Penland and published by . This book was released on 1960 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1 97 and Angles of Attack Up to 90

Download or read book Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1 97 and Angles of Attack Up to 90 written by Gerald V. Foster and published by . This book was released on 1961 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal  Directional  and Lateral Stability and Control Data at a Mach Number of 6 83 of the Final Configuration of the X  15 Research Airplane

Download or read book Static Longitudinal Directional and Lateral Stability and Control Data at a Mach Number of 6 83 of the Final Configuration of the X 15 Research Airplane written by and published by . This book was released on 1960 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Stability and Control Characteristics at Mach Numbers of 2 50  3 00  and 3 71 of a Variable  Wing sweep Configuration with Outboard Wing Panels Swept Back 75

Download or read book Stability and Control Characteristics at Mach Numbers of 2 50 3 00 and 3 71 of a Variable Wing sweep Configuration with Outboard Wing Panels Swept Back 75 written by Gerald V. Foster and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Stability and Control Characteristics at Mach Numbers of 2 50  3 00  and 3 71 of a Variable  Wing sweep Configuration with Outboard Wing Panels Swept Back 75 Deg

Download or read book Stability and Control Characteristics at Mach Numbers of 2 50 3 00 and 3 71 of a Variable Wing sweep Configuration with Outboard Wing Panels Swept Back 75 Deg written by and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0 80 Chord Line Unswept and with Several Tail Configurations

Download or read book Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0 80 Chord Line Unswept and with Several Tail Configurations written by Kenneth W. Goodson and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The basic aspect-ratio-4.00 wing had a zero taper and an unswept 0.80 chord line. Several aspect-ratio modifications to the basic wing were made by clipping off portions of the wing tips. The complete model was tested with a chord-plane tail, a T-tail, and a biplane tail (combined T-tail and chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92. The data show that, when reduced to the same static margin, all the tail configurations tested on the model provided fairly good stability characteristics, the biplane tail giving the best overall characteristics as regards pitching-moment linearity. Changes in static margin at zero lift coefficient with Mach number were small for the model with these tails over the Mach number range investigated.

Book Static Longitudinal and Lateral Stability Characteristics at Mach Number of 3 11 of Square and Circular Plan form Reentry Vehicles with Some Effects of Controls and Leading edge Extensions  with List of References

Download or read book Static Longitudinal and Lateral Stability Characteristics at Mach Number of 3 11 of Square and Circular Plan form Reentry Vehicles with Some Effects of Controls and Leading edge Extensions with List of References written by and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: