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Book Ditching Tests with a 1 10 size Model of the Army A 20A Airplane in Langley Tank No  2 and on an Outdoor Catapult

Download or read book Ditching Tests with a 1 10 size Model of the Army A 20A Airplane in Langley Tank No 2 and on an Outdoor Catapult written by George A. Jarvis and published by . This book was released on 1944 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests with a dynamically similar model of the army A-20A airplane were made to determine the best way to land the airplane in calm and rough water and to determine its probable ditching performance. The behavior was studied by making visual operations, by recording longitudinal decelerations, and by taking motion pictures of the landings.

Book Ditching Tests with a 1 16 size Dynamic Model of the Army B 24 Airplane in Langley Tank No  2 and on an Outdoor Catapult

Download or read book Ditching Tests with a 1 16 size Dynamic Model of the Army B 24 Airplane in Langley Tank No 2 and on an Outdoor Catapult written by Lloyd J. Fisher and published by . This book was released on 1945 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted to determine the best way to ditch the Army B-24 airplane in calm and rough water and to determine its probable ditching performance. A dynamically similar mode of the B-24 airplane was ditched in calm water in tank no. 2 and in calm and rough water from an outdoor catapult. Its behavior was ascertained by making visual observations, by recording maximum decelerations, and by taking motion-picture records of the landings.

Book Ditching Tests with 1 16 size Models of the Army B 17 Airplane in Langley Tank No  2 and on an Outdoor Catapult

Download or read book Ditching Tests with 1 16 size Models of the Army B 17 Airplane in Langley Tank No 2 and on an Outdoor Catapult written by Robert P. Tarshis and published by . This book was released on 1945 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests with dynamically similar models were made to study the behavior of the Army B-17F and B-17G airplanes when ditched and to determine the best way to land them in calm and rough water. The models were ditched in calm water from the tank no. 2 towing carriage and in calm and rough water from an outdoor catapult.

Book Bibliography of Scientific and Industrial Reports

Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1948 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Ditching Tests with a 1 12 size Model of the Army B 26 Airplane in NACA Tank No  2 and on an Outdoor Catapult

Download or read book Ditching Tests with a 1 12 size Model of the Army B 26 Airplane in NACA Tank No 2 and on an Outdoor Catapult written by Lloyd J. Fisher and published by . This book was released on 1944 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were made at the Langley Memorial Aeronautical Laboratory with a 1/12-size dynamic model of the Army B-26 airplane to determine its behavior when landed on water.

Book Ditching Tests of a 1 8 size Model of the Navy SB2C 1 Airplane  Army A 25  in Langley Tank No  2 and on an Outdoor Catapult

Download or read book Ditching Tests of a 1 8 size Model of the Navy SB2C 1 Airplane Army A 25 in Langley Tank No 2 and on an Outdoor Catapult written by George A. Jarvis and published by . This book was released on 1946 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Ditching Tests with a 1 11 size Model of the Army B 25 Airplane in NACA Tank No  2 and on an Outdoor Catapult

Download or read book Ditching Tests with a 1 11 size Model of the Army B 25 Airplane in NACA Tank No 2 and on an Outdoor Catapult written by George A. Jarvis and published by . This book was released on 1944 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were made to determine the best way to land the B-25 airplane in calm and rough water and to determine its probable ditching performance. A dynamically similar mode of the B-25 airplane was landed in calm water in tank no. 2 and in calm and rough water from the outdoor catapult. Its behavior was determined by making visual observations, by recording longitudinal accelerations, and by taking motion pictures of the landings.

Book Ditching Tests with a 1 10 size Model of the Army A 20A Airplane

Download or read book Ditching Tests with a 1 10 size Model of the Army A 20A Airplane written by John R. Dawson and published by . This book was released on 1943 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: The tests reported herein are the first in a series of tests requested by the Army Air Forces to determine the behavior of landplanes when they are forced to land on the water. (The emergency landing of a landplane on water is called "ditching.") The tests are being made in NACA tank no. 2 with scale dynamic models (models having scale weight and scale moment of inertia about all axes).

Book Bibliography of Scientific and Industrial Reports

Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1948 with total page 1300 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Ditching Tests of a 1 20 Scale Model of the Northrop B 35 Airplane

Download or read book Ditching Tests of a 1 20 Scale Model of the Northrop B 35 Airplane written by Lloyd J. Fisher and published by BiblioGov. This book was released on 2013-07 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests of a 1/20-scale dynamically similar model of the Northrop B-35 airplane were made to study its ditching characteristics. The model was ditched in calm water at the Langley tank no. 2 monorail. Various landing attitudes, speeds, and conditions of damage were simulated during the investigation. The ditching characteristics were determined by visual observation and from motion-picture records and time-history acceleration records. Both longitudinal and lateral accelerations were measured. Results are given in tabular form and time-history acceleration curves and sequence photographs are presented. Conclusions based on the model investigation are as follows: 1. The best ditching of the B-35 airplane probably can be made by contacting the water in a near normal landing attitude of about 9 deg with the landing flaps full down so as to have a low horizontal speed. 2. The airplane usually will turn or yaw but the motion will not be violent. The maximum lateral acceleration will be about 2g. 3. If the airplane does not turn or yaw immediately after landing, it probably will trim up and then make a smooth run or porpoise slightly. The maximum longitudinal decelerations that will be encountered are about 6g or 7g. 4. Although the decelerations are not indicated to be especially large, the construction of the airplane is such that extensive damage is to be expected, and it probably will be difficult to find ditching stations where crew members can adequately brace themselves and be reasonably sure of avoiding a large inrush of water

Book Ditching Tests of a 1 24 Scale Model of the Lockheed Xr60 1 Airplane  Ted No  Naca 235

Download or read book Ditching Tests of a 1 24 Scale Model of the Lockheed Xr60 1 Airplane Ted No Naca 235 written by Nasa Technical Reports Server (Ntrs) and published by BiblioGov. This book was released on 2013-07 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The ditching characteristics of the Lockheed XR60-1 airplane were determined by tests of a 1/24-scale dynamic model in calm water at the Langley tank no. 2 monorail. Various landing attitudes, flap settings, speeds, and conditions of damager were investigated. The ditching behavior was evaluated from recordings of decelerations, length of runs, and motions of the model. Scale-strength bottoms and simulated crumpled bottoms were used to reproduce probable damage to the fuselage. It was concluded that the airplane should be ditched at a landing attitude of about 5 deg with flaps full down. At this attitude, the maximum longitudinal deceleration should not exceed 2g and the landing run will be bout three fuselage lengths. Damage to the fuselage will not be excessive and will be greatest near the point of initial contact with the water.

Book The Evolution of the Cruise Missile

Download or read book The Evolution of the Cruise Missile written by Kenneth P. Werrell and published by . This book was released on 1985 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Hydrodynamics of High Speed Marine Vehicles

Download or read book Hydrodynamics of High Speed Marine Vehicles written by Odd M. Faltinsen and published by Cambridge University Press. This book was released on 2006-01-09 with total page 490 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hydrodynamics of High-Speed Marine Vehicles, first published in 2006, discusses the three main categories of high-speed marine vehicles - vessels supported by submerged hulls, air cushions or foils. The wave environment, resistance, propulsion, seakeeping, sea loads and manoeuvring are extensively covered based on rational and simplified methods. Links to automatic control and structural mechanics are emphasized. A detailed description of waterjet propulsion is given and the effect of water depth on wash, resistance, sinkage and trim is discussed. Chapter topics include resistance and wash; slamming; air cushion-supported vessels, including a detailed discussion of wave-excited resonant oscillations in air cushion; and hydrofoil vessels. The book contains numerous illustrations, examples and exercises.

Book Cave of the Winds

    Book Details:
  • Author : Joseph R. Chambers
  • Publisher : NASA
  • Release : 2014
  • ISBN : 9781626830165
  • Pages : 533 pages

Download or read book Cave of the Winds written by Joseph R. Chambers and published by NASA. This book was released on 2014 with total page 533 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Above the Pacific

Download or read book Above the Pacific written by William Joseph Horvat and published by . This book was released on 1966 with total page 234 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book American Airpower Comes Of Age   General Henry H     Hap    Arnold   s World War II Diaries Vol  II  Illustrated Edition

Download or read book American Airpower Comes Of Age General Henry H Hap Arnold s World War II Diaries Vol II Illustrated Edition written by Gen. Henry H. “Hap.” Arnold and published by Pickle Partners Publishing. This book was released on 2015-11-06 with total page 927 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Aerial Warfare In Europe During World War II illustrations pack with over 180 maps, plans, and photos. Gen Henry H. “Hap.” Arnold, US Army Air Forces (AAF) Chief of Staff during World War II, maintained diaries for his several journeys to various meetings and conferences throughout the conflict. Volume 1 introduces Hap Arnold, the setting for five of his journeys, the diaries he kept, and evaluations of those journeys and their consequences. General Arnold’s travels brought him into strategy meetings and personal conversations with virtually all leaders of Allied forces as well as many AAF troops around the world. He recorded his impressions, feelings, and expectations in his diaries. Maj Gen John W. Huston, USAF, retired, has captured the essence of Henry H. Hap Arnold—the man, the officer, the AAF chief, and his mission. Volume 2 encompasses General Arnold’s final seven journeys and the diaries he kept therein.