Download or read book Transonic Longitudinal and Lateral Aerodynamic Characteristics of a Preliminary Concept of a First stage Horizontal take off And horizontal landing Recoverable Booster with a 70 Deg Delta Wing written by and published by . This book was released on 1962 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Longitudinal and Lateral Aerodynamic Characteristics of a Preliminary Concept of a First Stage Horizontal Take Off and Horizontal Landing Recoverable Booster with a 70 Delta Wing written by P. Kenneth Pierpont and published by . This book was released on 1962 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Aerodynamic Characteristics of a Horizontal Take off and Landing Reusable Booster Having Variations in Wing Planform written by and published by . This book was released on 1964 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Aerodynamic Characteristics of a Lifting Reentry Vehicle Having a Delta Planform and a Flat Bottom written by and published by . This book was released on 1965 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics at Transonic and Supersonic Speeds of a Rocket propelled Airplane Configuration Having a 52 5 Degree Delta Wing and a Low Swept Horizontal Tail written by Alan B. Kehlet and published by . This book was released on 1954 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2 01 of a Tailless Delta V STOL Configuration Having Variable sweep Wing Panels written by and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Design Guide for Pitch up Evaluation and Investigation at High Subsonic Speeds of Possible Limitations Due to Wing aspect ratio Variations written by Kenneth P. Spreemann and published by . This book was released on 1959 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High Supersonic Lateral Directional Stability Characteristics of a 70 Deg Swept Wing body tail Model with Various Body Cross Sectional Shapes written by and published by . This book was released on 1964 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Aerodynamic Characteristics of the Dyna soar Glider and Titan 3 Launch Vehicle Configuration with Various Fin Arrangements written by and published by . This book was released on 1963 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Ground Proximity on Aerodynamic Characteristics of Two Horizontal Attitude Jet Vertical Take Off and Landing Airplane Models written by William A. Newsom (Jr) and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made to study the effect of ground proximity on the aerodynamic characteristics of two jet vertical-take-off-and-landing airplane models in which the fuselage remains in a horizontal attitude for the take-off and landing. The first model (called the tilt-wing model) had a tilting wing-engine assembly which was set at 90 deg incidence for the take-off and landing. The second model, called the deflected-jet model) had a cascade of retractable turning vanes to deflect the exhaust of the horizontally mounted jet engines downward for vertical take-off and landing while the entire model remained in a horizontal attitude. With the models at various heights above the ground in the take-off and landing configuration, the lift, drag, and pitching moment were measured and tuft surveys were made to determine the flow field caused by the jet exhaust. The tilt-wing model experienced a loss of lift of less than 3 percent near the ground. The deflected-jet model, however, suffered losses in lift as high as 45 percent near the ground because of a low pressure region under the model caused by the entrainment of air by the jet exhaust as it spread out along the ground. This loss in lift for the deflected-jet configuration could probably be reduced to less than 5 percent by the use of a longer landing gear and a high wing location.
Download or read book Effects of Landing Gear Speed Brake and Protuberances on the Longitudinal Aerodynamic Characteristics of an NASA Supercritical wing Research Airplane Model written by and published by . This book was released on 1975 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Characteristics at Transonic and Supersonic Speeds of a Rocket propelled Airplane Model Having a 60 Degrees Wing and a Low Swept Horizontal Tail written by Robert F. Peck and published by . This book was released on 1955 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Effects of Five Lift fan Pod Arrangements on an Unpowered V STOL Transport Model written by James Lee Thomas and published by . This book was released on 1973 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Studies of Stability and Control of Winged Reentry Configurations written by and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect on to Ground Proximity Aerodynamic Characteristics of Two Horizontal attitude Checked Vertical take off and landing Airplane Models written by and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made to study the effects of ground proximity on the aerodynamic characteristics of two jet vertical-take-off-and-landing. The first model (public tilt-wing model) had a tilting wing-engine assembly which was set at 90 degrees incidence for the take-off and landing. The second model (called the deflected-jet model) had a cascade of retractable turning vanes to deflect take-off and landing while the entire model remained in a horizontal attitude. With the models at various heights above the ground in the take-off and landing configuration, the lift, drag, and pitching moments were measured and tuft surveys were made to determine the flow field caused by the jet exhaust. The tilt-winged model experienced a loss of left or less than 3 percent near the ground. The deflected-jet model, however, suffered losses in lift as high as 45 percent near the ground because of a low pressure region under the model caused by the entrainment of air by the jet exhaust as it spread adults along the ground. This loss in an lift for the deflected-jet configuration could probably be reduced to less than 5 percent by the use of a longer landing gear and a high wing location.
Download or read book From Archangel to Senior Crown written by Peter W. Merlin and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2008 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Lockheed Blackbirds hold a unique place in the development of aeronautics. In their day, the A-12, YF-12, M-21, D-21, and SR-71 variants outperformed all other jet airplanes in terms of altitude and speed. Now retired, they remain the only production aircraft capable of sustained Mach 3 cruise and operational altitudes above 80,000 feet.This is the first book to address the technical aspects of these incredible aircraft. The author describes the design evolution of the Blackbird, from the Archangel to the Senior Crown (the Air Force's SR-71.) He describes in detail the construction and materials challenges faced by Lockheed, as well as the Blackbird's performance characteristics and capabilities.A NASA historian, the author describes NASA's role in using the aircraft as a flying laboratory to collect data on materials, structures, loads, heating, aerodynamics, and performance for high-speed aircraft. The reader will benefit from the technical and programmatic lessons learned.This volume was produced in cooperation with the National Aeronautics and Space Administration.
Download or read book Aerodynamic Characteristics Over a Mach Number Range of 1 40 to 2 78 of a Rocket propelled Airplane Configuration Having a Low 52 5 Degree Delta Wing and an Unswept Horizontal Tail written by Alan B. Kehlet and published by . This book was released on 1958 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
