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Wind Tunnel Investigation At Mach Numbers From 06 To 14 Of Several Ejected Pilot Seat Models
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Book Synopsis Wind-tunnel Investigation at Mach Numbers from 0.6 to 1.4 of Several Ejected Pilot-seat Models by : James L. Summers
Download or read book Wind-tunnel Investigation at Mach Numbers from 0.6 to 1.4 of Several Ejected Pilot-seat Models written by James L. Summers and published by . This book was released on 1958 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the static longitudinal and lateral directional aerodynamic characteristics of basic and modified versions of a conventional upward ejected pilot-set combination, a sled-type upward ejected pilot-seat combination, and a downward ejected pilot-seat combination. Modifications of the basic models incorporated flow deflectors for pilot protection and drag reduction and various stabilizing devices. Test Mach numbers varied from 0.6 to 1.4, angles of attack from -28 to 40 degrees, and angles of sideslip from -16 to 12 degrees. Reynolds numbers ranged from 0.9 million to 1.8 million based on the projected frontal height of the models.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1985 with total page 1076 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Analysis of Wind Tunnel Test of a 1/2 Scale Model of an Ejecting Crewman and Ejection Seat by : Alastair Anthony
Download or read book Preliminary Analysis of Wind Tunnel Test of a 1/2 Scale Model of an Ejecting Crewman and Ejection Seat written by Alastair Anthony and published by . This book was released on 1979 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Doubts were raised as to the integrity of the rest of the structure when the neck member of a model crewman failed during tunnel measurements of the limb forces during ejection. The accuracy of the load estimates used in the pretest stress analysis clearly needed to be checked. Meanwhile, testing was resumed at restricted pressure values with a non-load-measuring replacement for the neck member. From a sampling of the test data, the distribution of bending and torsional moments along the limbs is clearly revealed and, with its variation with attitude and Mach number, presents no great surprises. Values critical to the stress analysis confirm the estimated values. The neck pillar, designed by a subcontractor, had been designed for sensitivity in bending under the head loads without catering for torsion in the member if these load should in the event be appreciably offset from its axis. Although there is little confirmation of the magnitude of the head loads, there is some indication the offsets in excess of one inch in these loads are to be expected in the real situation, and that the resulting torsion was the cause of the failure. (Author).
Book Synopsis Investigation of Aerodynamic Effects of External Combustion Below Flat-plate Model in 10- by 10-foot Wind Tunnel at Mach 2.4 by : Robert G. Dorsch
Download or read book Investigation of Aerodynamic Effects of External Combustion Below Flat-plate Model in 10- by 10-foot Wind Tunnel at Mach 2.4 written by Robert G. Dorsch and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation of Nozzle Hinge Moments on Two Launch Vehicle Models at Mach Numbers 1.60, 2.00, and 2.40 by :
Download or read book Wind Tunnel Investigation of Nozzle Hinge Moments on Two Launch Vehicle Models at Mach Numbers 1.60, 2.00, and 2.40 written by and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 0.8 to 1.4 of Static Longitudinal and Lateral-directional Characteristics of an Unswept-wing Airplane Model by : James L. Summers
Download or read book Wind-tunnel Investigation at Mach Numbers from 0.8 to 1.4 of Static Longitudinal and Lateral-directional Characteristics of an Unswept-wing Airplane Model written by James L. Summers and published by . This book was released on 1956 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability and Control of Airplanes and Helicopters by : Edward Seckel
Download or read book Stability and Control of Airplanes and Helicopters written by Edward Seckel and published by Academic Press. This book was released on 2014-05-10 with total page 523 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stability and Control of Airplanes and Helicopters deals with aircraft flying qualities that determine the stability and control of airplanes and helicopters. It includes problems based on real aircraft, selected to represent the gamut from simple to complicated, and from conventional utility designs to futuristic research types. Many of these problems involve comparison of theory and experiment to demonstrate their mutual relationship. Comprised of 25 chapters, this book begins with a discussion on the aerodynamics of the component parts related to the lift and moment characteristics of an airplane, including wings and associated accessories; bodies such as fuselages, nacelles, and tip tanks; and control surfaces. The reader is then introduced to some mathematical techniques for linear differential equations; steady flight at different speeds; and stick force and control-free stability. Subsequent chapters focus on flaps and high-lift devices; power and compressibility effects; and the manner in which the aircraft responds to the application of control. Aeroelasticity and longitudinal equations of motion are also examined. This monograph is intended for undergraduate and graduate students taking modern engineering courses.
Download or read book Aero/space Engineering written by and published by . This book was released on 1959 with total page 814 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1965 with total page 914 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characteristics of a Possible Reentry Capsule by :
Download or read book Wind-tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characteristics of a Possible Reentry Capsule written by and published by . This book was released on 1960 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations by :
Download or read book Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations written by and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characterictics of a Possible Reentry Capsule by : Albin O. Pearson
Download or read book Wind Tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characterictics of a Possible Reentry Capsule written by Albin O. Pearson and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation of the Aerodynamic Characteristics of Five Forebody Models at High Angles of Attack at Mach Numbers from 0.25 to 2 by :
Download or read book Wind Tunnel Investigation of the Aerodynamic Characteristics of Five Forebody Models at High Angles of Attack at Mach Numbers from 0.25 to 2 written by and published by . This book was released on 1975 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Choking Mach Number in High Speed Wind Tunnel with Consideration of the Model Lift by : Bernhard A.. Goethert
Download or read book Choking Mach Number in High Speed Wind Tunnel with Consideration of the Model Lift written by Bernhard A.. Goethert and published by . This book was released on 1948 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 1.60 to 4.50 of the Static-stability Characteristics of Two Nonlifting Vehicles Suitable for Reentry by : Kenneth L. Turner
Download or read book Wind-tunnel Investigation at Mach Numbers from 1.60 to 4.50 of the Static-stability Characteristics of Two Nonlifting Vehicles Suitable for Reentry written by Kenneth L. Turner and published by . This book was released on 1959 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation of Capsule Ejections from the Side and Base of a Carrier Vehicle at Mach Numbers 2, 4, 5, and 8 by : L. A. MORGAN
Download or read book Wind Tunnel Investigation of Capsule Ejections from the Side and Base of a Carrier Vehicle at Mach Numbers 2, 4, 5, and 8 written by L. A. MORGAN and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted in the 40-Inch Supersonic and 50-Inch Mach 8 Tunnels of the von Karman Gas Dynamics Facility to determine the separation characteristics of ejected capsules while in the influence of the flow field of the carrier vehicle. High-speed movies were obtained of cylindrical and cone-cylinder flared capsules ejected at Mach numbers 2, 4, 5, and 8 with a constant free-stream Reynolds number of 3.4 x 10 to the 6th power per ft. The capsule orientations along their trajectories are presented to illustrate the results obtained. (Author).
Book Synopsis Bibliography of Scientific and Industrial Reports by :
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1946 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
