Flights from the Deep
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Long Night of the Tankers: Hitler’S War Against Caribbean Oil
University of Calgary PRISM: University of Calgary's Digital Repository University of Calgary Press University of Calgary Press Open Access Books 2014 Long Night of the Tankers: Hitler’s War Against Caribbean Oil Bercuson, David J.; Herwig, Holger H. University of Calgary Press Bercuson, D. J. & Herwig, H. H. "Long Night of the Tankers: Hitler’s War Against Caribbean Oil". Beyond Boundaries: Canadian Defence and Strategic Studies Series; 4. University of Calgary Press, Calgary, Alberta, 2014. http://hdl.handle.net/1880/49998 book http://creativecommons.org/licenses/by-nc-nd/4.0/ Attribution Non-Commercial No Derivatives 4.0 International Downloaded from PRISM: https://prism.ucalgary.ca University of Calgary Press www.uofcpress.com LONG NIGHT OF THE TANKERS: HITLER’S WAR AGAINST CARIBBEAN OIL David J. Bercuson and Holger H. Herwig ISBN 978-1-55238-760-3 THIS BOOK IS AN OPEN ACCESS E-BOOK. It is an electronic version of a book that can be purchased in physical form through any bookseller or on-line retailer, or from our distributors. Please support this open access publication by requesting that your university purchase a print copy of this book, or by purchasing a copy yourself. If you have any questions, please contact us at [email protected] Cover Art: The artwork on the cover of this book is not open access and falls under traditional copyright provisions; it cannot be reproduced in any way without written permission of the artists and their agents. The cover can be displayed as a complete cover image for the purposes of publicizing this work, but the artwork cannot be extracted from the context of the cover of this specific work without breaching the artist’s copyright. -
U.S. Gato Class 26 Submarine Us Navy Measure 32/355-B
KIT 0384 85038410200 GENERAL HULL PAINT GUIDE U.S. GATO CLASS 26 SUBMARINE US NAVY MEASURE 32/355-B In the first few months immediately following the Japanese attack on surface and nine knots under water. Their primary armament consisted Pearl Harbor, it was the U. S. Navy’s submarine force that began unlimited of twenty-four 21-inch torpedoes which could be fired from six tubes in the warfare against Japan. While the surfaces forces regrouped, the submarines bow and four in the stern. Most GATO class submarines typically carried began attacking Japanese shipping across the Pacific. Throughout the war, one 3-inch, one 4-inch, or one 5-inch deck gun. To defend against aircraft American submarines sunk the warships of the Imperial Japanese Navy and while on the surface, one or two 40-mm guns were usually fitted, and cut the lifeline of merchant vessels that provided Japan with oil and other these were supplemented by 20mm cannon as well as .50 caliber and vital raw materials. They also performed other important missions like staging .30 caliber machine guns. Gato class subs were 311'9" long, displaced commando raids and rescuing downed pilots. The most successful of the 2,415 tons while submerged, and carried a crew of eighty-five men. U. S. fleet submarines during World War II were those of the GATO class. Your hightly detailed Revell 1/72nd scale kit can be used to build one of Designed to roam the large expanses of the Pacific Ocean, these submarines four different WWII GATO class submarines: USS COBIA, SS-245, USS were powered by two Diesel engines, generating 5,400 horse power for GROWLER, SS-215, USS SILVERSIDES, SS-236, and the USS FLASHER, operating on the surface, and batteries provided power while submerged. -
A Brief Review on Electromagnetic Aircraft Launch System
International Journal of Mechanical And Production Engineering, ISSN: 2320-2092, Volume- 5, Issue-6, Jun.-2017 http://iraj.in A BRIEF REVIEW ON ELECTROMAGNETIC AIRCRAFT LAUNCH SYSTEM 1AZEEM SINGH KAHLON, 2TAAVISHE GUPTA, 3POOJA DAHIYA, 4SUDHIR KUMAR CHATURVEDI Department of Aerospace Engineering, University of Petroleum and Energy Studies, Dehradun, India E-mail: [email protected] Abstract - This paper describes the basic design, advantages and disadvantages of an Electromagnetic Aircraft Launch System (EMALS) for aircraft carriers of the future along with a brief comparison with traditional launch mechanisms. The purpose of the paper is to analyze the feasibility of EMALS for the next generation indigenous aircraft carrier INS Vishal. I. INTRODUCTION maneuvering. Depending on the thrust produced by the engines and weight of aircraft the length of the India has a central and strategic location in the Indian runway varies widely for different aircraft. Normal Ocean. It shares the longest coastline of 7500 runways are designed so as to accommodate the kilometers amongst other nations sharing the Indian launch for such deviation in takeoff lengths, but the Ocean. India's 80% trade is via sea routes passing scenario is different when it comes to aircraft carriers. through the Indian Ocean and 85% of its oil and gas Launch of an aircraft from a mobile platform always are imported through sea routes. Indian Ocean also requires additional systems and methods to assist the serves as the locus of important international Sea launch because the runway has to be scaled down, Lines Of Communication (SLOCs) . Development of which is only about 300 feet as compared to 5,000- India’s political structure, industrial and commercial 6,000 feet required for normal aircraft to takeoff from growth has no meaning until its shores are protected. -
Adventures in Low Disk Loading VTOL Design
NASA/TP—2018–219981 Adventures in Low Disk Loading VTOL Design Mike Scully Ames Research Center Moffett Field, California Click here: Press F1 key (Windows) or Help key (Mac) for help September 2018 This page is required and contains approved text that cannot be changed. NASA STI Program ... in Profile Since its founding, NASA has been dedicated • CONFERENCE PUBLICATION. to the advancement of aeronautics and space Collected papers from scientific and science. The NASA scientific and technical technical conferences, symposia, seminars, information (STI) program plays a key part in or other meetings sponsored or co- helping NASA maintain this important role. sponsored by NASA. The NASA STI program operates under the • SPECIAL PUBLICATION. Scientific, auspices of the Agency Chief Information technical, or historical information from Officer. It collects, organizes, provides for NASA programs, projects, and missions, archiving, and disseminates NASA’s STI. The often concerned with subjects having NASA STI program provides access to the NTRS substantial public interest. Registered and its public interface, the NASA Technical Reports Server, thus providing one of • TECHNICAL TRANSLATION. the largest collections of aeronautical and space English-language translations of foreign science STI in the world. Results are published in scientific and technical material pertinent to both non-NASA channels and by NASA in the NASA’s mission. NASA STI Report Series, which includes the following report types: Specialized services also include organizing and publishing research results, distributing • TECHNICAL PUBLICATION. Reports of specialized research announcements and feeds, completed research or a major significant providing information desk and personal search phase of research that present the results of support, and enabling data exchange services. -
Flow Visualization Studies of VTOL Aircraft Models During Hover in Ground Effect
NASA Technical Memorandum 108860 Flow Visualization Studies of VTOL Aircraft Models During Hover In Ground Effect Nikos J. Mourtos, Stephane Couillaud, and Dale Carter, San Jose State University, San Jose, California Craig Hange, Doug Wardwell, and Richard J. Margason, Ames Research Center, Moffett Field, California Janua_ 1995 National Aeronautics and Space Administration Ames Research Center Moffett Field, California 94035-1000 Flow Visualization Studies of VTOL Aircraft Models During Hover In Ground Effect NIKOS J. MOURTOS,* STEPHANE COUILLAUD,* DALE CARTER,* CRAIG HANGE, DOUG WARDWELL, AND RICHARD J. MARGASON Ames Research Center Summary fountain fluid flows along the fuselage lower surface toward the jets where it is entrained by the jet and forms a A flow visualization study of several configurations of a vortex pair as sketched in figure 1(a). The jet efflux and jet-powered vertical takeoff and landing (VTOL) model the fountain flow entrain ambient temperature air which during hover in ground effect was conducted. A surface produces a nonuniform temperature profile. This oil flow technique was used to observe the flow patterns recirculation is called near-field HGI and can cause a on the lower surfaces of the model. Wing height with rapid increase in the inlet temperature which in turn respect to fuselage and nozzle pressure ratio are seen to decreases the thrust. In addition, uneven temperature have a strong effect on the wing trailing edge flow angles. distribution can result in inlet flow distortion and cause This test was part of a program to improve the methods compressor stall. In addition, the fountain-induced vortex for predicting the hot gas ingestion (HGI) for jet-powered pair can cause a lift loss and a pitching-moment vertical/short takeoff and landing (V/STOL) aircraft. -
Supersonic STOVL Ejector Aircraft from a Propulsion Point of View
N84-24581 NASA Technical Memorandum 83641 9 Supersonic STOVL Ejector Aircraft from a Propulsion Point of View R. Luidens, R. Plencner, W. Haller, and A. blassman Lewis Research Center Cleveland, Ohio Prepared for the Twentieth Joint Propulsion Coiiference cosponsored by the AIAA, SAE, and ASME i Cincinnati, Ohio, June 11-13, 1984 I 1 1 SUPERSONIC STOVL EJECTOR AIRCRAFT FROH A PROPULSION POINT OF VIEW R hidens,* R. Plencner,** W. Hailer.** and A Glassman+ National Aeronautics and Space Administration Lewis Research Center Cleveland, Ohio Abstract 1 Higher propulsion system thrust for greater lift-off acceleration. The paper first describes a baseline super- sonic STOVL ejector aircraft, including its 2 Cooler footprint, for safer, more propulsion and typical operating modes, and convenient handllng, and lower observability identiftes Important propulsion parameters Then a number of propulsion system changes are 3. Alternattve basic propulsion cycles evaluated in terms of improving the lift-off performance; namely, aft deflection of the ejec- The approach of this paper is to use the tor jet and heating of the ejector primary air aircraft of reference 5 as a baseline. and then either by burning or using the hot englne core to consider some candidate propulsion system flow The possibility for cooling the footprint growth options The vehicle described in refe- is illustrated for the cases of mixing or lnter- rence 5 was selected on the basis of detailed changlng the fan and core flows, and uslng a alrcraft design and performance analyses The -
Modeling and Analysis of Disc Rotor Wing
© 2020 JETIR March 2020, Volume 7, Issue 3 www.jetir.org (ISSN-2349-5162) MODELING AND ANALYSIS OF DISC ROTOR WING 1 2 3 G. MANJULA , L. BALASUBRAMANYAM , S. JITHENDRA NAIK 1PG scholor, 2Asso.Professor, 3Asso.Professor Mechanical Engineering Department 1P.V.K.K Engineering College, Anantapur, AP, INDIA. Abstract-Disc rotor configuration may be a conceptual design. the aim of the Project is to guage the merits of the DiscRotor concept that combine the features of a retractable rotor system for vertical take-off and landing (VTOL) with an integral, circular wing for high-speed flight. The primary objective of this project is to style such a configuration using the planning software Unigraphics and afterward analyzing the designed structure for its structural strength in analysis software ANSYS. This project deals with the all the required aerodynamic requirements of the rotor configuration. In today’s world most the vtol/stol largely depends upon the thrust vectoring that needs huge amounts of fuel and separate devices like nozzles etc., whose production is extremely much tedious and dear. this is often an effort to use a rotor as within the case of helicopters for vtol/stol thus reducing the foremost of the value though weight would be considered as a hindrance to the project. Keywords: Disc rotor wing, vertical take-off and landing (VTOL), UNIGRAPHICS, ANSYS software, Force, Coefficients, Wall and Wing. I. INTRODUCTION A circular wing, or disc, is that the primary lifting surface of the Disc Rotor aircraft during high-speed flight (approx. 400knots). During the high-speed flight, the disc are going to be fixed (i.e. -
The Third Battle
NAVAL WAR COLLEGE NEWPORT PAPERS 16 The Third Battle Innovation in the U.S. Navy's Silent Cold War Struggle with Soviet Submarines N ES AV T A A L T W S A D R E C T I O N L L U E E G H E T R I VI IBU OR A S CT MARI VI Owen R. Cote, Jr. Associate Director, MIT Security Studies Program The Third Battle Innovation in the U.S. Navy’s Silent Cold War Struggle with Soviet Submarines Owen R. Cote, Jr. Associate Director, MIT Security Studies Program NAVAL WAR COLLEGE Newport, Rhode Island Naval War College The Newport Papers are extended research projects that the Newport, Rhode Island Editor, the Dean of Naval Warfare Studies, and the Center for Naval Warfare Studies President of the Naval War College consider of particular Newport Paper Number Sixteen interest to policy makers, scholars, and analysts. Candidates 2003 for publication are considered by an editorial board under the auspices of the Dean of Naval Warfare Studies. President, Naval War College Rear Admiral Rodney P. Rempt, U.S. Navy Published papers are those approved by the Editor of the Press, the Dean of Naval Warfare Studies, and the President Provost, Naval War College Professor James F. Giblin of the Naval War College. Dean of Naval Warfare Studies The views expressed in The Newport Papers are those of the Professor Alberto R. Coll authors and do not necessarily reflect the opinions of the Naval War College or the Department of the Navy. Naval War College Press Editor: Professor Catherine McArdle Kelleher Correspondence concerning The Newport Papers may be Managing Editor: Pelham G. -
Forwards "Mgt & Technical Resources,Jul 1979," Per NRC 790629 Info
N L MONTICELLO NUCLEAR GENERATING PLANT PRAIRIE I SLAND NUCLEAR GENERATING PLANT RETU TO RT 7R0 ET J\~FIES -+4c6Z010 3 19 FEt T DCKET NSP MANAGEMENT &TECHNICAL RESOURCES JULY. 1979 RETU1 TO ETBR DOCKET A RILES I NORTHERN STATES POWER COMPANY MINNEAPOLIS. MINNESOTA o908210'34 ? MSP NORTHERN STATES POWER COMPANY MINNEAPOLIS. MINNESOTA 55401 August 10, 1979 Director of Nuclear Reactor Regulation US Nuclear Regulatory Commission Washington, DC 20555 MONTICELLO NUCLEAR GENERATING PLANT PRAIRIE ISLAND NUCLEAR GENERATING PLANT Docket Nos. 50-263 License Nos. DPR-22 50-282 DPR-42 50-306 DPR-60 Response to NRC Request for Information on Management and Technical Resources Your letter dated June 29, 1979 requested information on management and technical resources available to licensees for response to nuclear plant emergencies. A subsequent letter from W P Haass, Chief, Quality Assurance Branch, requested that we submit a total of 50 copies of the requested information based upon NSP operating three units. Attached are 50 copies of a document entitled "NSP Management & Technical Resources, July, 1979". Should you have any questions on this document, please contact the undersigned at (612) 330-6078. L 0 Mayer, PE Manager of Nuclear Support Services LOM/jh cc: W P Haass (w/o attachment) J G Keppler NORTHERN STATES POWER COMPANY MANAGEMENT & TECHNICAL RESOURCES JHOY. 1979 1.0 Management Resources (offsite) 1.1 Summary 1.2 Organization Diagram 1.3 Mission Statements 1.4 Personnel Resume's 2.0 Technical Resources (plant staff) 2.1 Summary 2.2 Monticello -
History News Issue.341 April 2019
HISTORY NEWS ISSUE.341 APRIL 2019 INSIDE THIS ISSUE President’s Report What’s On 2019 AGM Japanese Reconnaissance Flight Frances Barkman Norma Mullins Lucy Bracey Eaglehawk Mechanics Institute Heritage Report Art Captured Victoria House Around the Societies Books received History Victoria Bookshop Prisoner at Camp 13 Annual AGL Shaw Lecture in partnership with the C J La Trobe President’s Report Society: RHSV NEWS RHSV ‘Garryowen: The Voice of Early Melbourne’ by Dr Liz Rushen, Chair History Council of Victoria I am writing this from History House. I draw the attention of all members to the RHSV has long aspired to develop the notice of the Annual General Meeting Tuesday 16 April 2019, 6.30 for 7pm Drill Hall as Melbourne’s History House, that is to be held on Tuesday 21 May. RHSV Offi cers’ Mess Upstairs and in its March meeting Council agreed One important aspect of the evening will This lecture will explore how Edmund Finn’s that we should start using the title on our be consideration of a several changes to 1888 impressions of pre-1851 Melbourne letterhead, website, etc, as a small start in the RHSV Constitution. These are mainly shaped what people understood to be achieving our ambition. updates to recognise current practices relevant, important, democratic, and even As reported previously, we have been (such as the use of email addresses, and Victorian. focusing on strengthening the RHSV membership renewal via the website) Note to RHSV members: this is not a free Council, and the RHSV Foundation. It and clarifi cation of matters such as the event and bookings are available through is critical that the Foundation is able to capacity of the Council to make By-Laws. -
Gato Class Submarine Specifications
1 Prepared by a former Mare Island yardbird, in memory of those who have gone before him 2 Gat o Class Submarine Specificat ions z Displace ment: 1,526 tons surfaced/2,424 tons submerged z Length: 311 feet, beam 27 feet, draft 15 feet z Speed: 20+ knots surfaced, 8+ knots submerged z Crew: 6 officers/54 men (10 officers/70-71 men wartime) z Maximum operating depth: 300 feet z Fuel capacity: 94,400 gals (116,000 gals wartime) z Patrol endurance: 75 days z Cruising range: 11,000 miles @ 10 knots (surfaced) z Submerged endurance: 48 hours @ 2 knots z A rma me nt : 10 torpedo tubes (6 fwd/4 aft), 21 torpedoes z Gun armament: 3-inch (later 4-inch), 20mm, and .50 caliber z Power plant: 4 diesel generators, 5,400 total horsepower z Propulsion: twin shaft, electric motors, two 126-cell batteries 3 Gato Class Internal Arrangement 4 Combat History of USS Wahoo z Seven war patrols z Credited with sinking 27 ships totaling over 125,000 tons z Earned 6 battle stars and awarded a Presidential Unit Citation z Commanded by CDR Dudley W. “Mush” Morton on last five patrols z One of 52 U.S. submar ines lost in WWII z Wahoo and other U.S. submarines completed 1,560 war patrols and sank over 5.6 million tons of Japanese shipping Wahoo patch & battle flag 5 Keel Laying - 28 June 1941 6 Wahoo Pressure Hull Sect ions - 1941 7 Under Construction on Building Way - January 1942 8 Launching Day - 14 February 1942 9 Launching Sponsor - Mrs. -
VIETNAMESE PRESIDENT UNHURT in ATTACK Vandenberg AIR FORCE BASE, Calif., FEB
HIGH TIDE lOW TIDE 3/1/62 3.9 AT 1156 3/1/62 2.3 AT 0444 3/2/62 3.4 AT 0103 RGLASS 3/1/62 2.1 AT 1912 VOL. 3 No. 1055 KWAJALEIN MARSHAll iSLANDS WEDNESDAY 28 fEBRUARY I 62 DISCOVERER NOo 38 SENT INTO ORBIT FROM VANDENBERG VIETNAMESE PRESIDENT UNHURT IN ATTACK VANDeNBeRG AIR FORCE BASE, CALif., FEB. 27 (UPi)-DISCOVERER No. 38 SATEL SAIGON, FEB. 27 (UPI)-THE PRESIDENTIAL PALACE WAS BOMBI' AND STRAfED BY LITE WAS HURLED INTO POLAR ORBIT TO fOUR VIETNAMESE AIR FORCE PLANES TODAY BUT PRESiDENT NGG DINH DIEM AND HIS DAY fROM THIS PACIFIC MISSILE RANGE FAMILY ESCAPED UNHURT. BASE, MARKING COMPLETION OF THREE DIEM, IN A STATEMENT OVER RADIO SAIGON SAID: YEARS IN THIS SPACE INFORMATION PRO "THANKS TO DIViNE PROTECTION i MYSELF AND MY CLOSE COLLABORATORS WERE NOT GRAM. IN DANGER. WE SUffERED ONLY MATERIAL DAMAGE." No. 38, CARRYING AN INSTRUMENT ALL AIR FORCE BASES WERE ALERTED AND ALL MEASURES Of SECURITY WERE TAKEN. PACKAGE CONTAINING UNDISCLOSED EXPERI ALL OffiCERS WERE TO fUNCTION NORMALLY AND THE POPULATION SHOULD REMAIN CALM MENTS, WAS LAUNCHED AT 11.39 A.M. AND fULFILL TrlEIR DUTIES. PST ( 9 39 A.M. HST) AND AN HOUR AND THE PRESIDENT LEFT SAIGON ON A "REGULARLY SCHEDULED TRIP" AT 0805 SAIGON A HALF LATER THE AIR fORCE RECEIVED TIME (0015 GMT). IT WAS NOT KNOWN EXACTLY WHERE HE WENT. WORD FROM TRACKING STATIONS IN HAWAI I THE PLANE'S PILOT, IDENTifiED AS LIEUTENANT PHAM PHO UOC, LANDED SAFf:L YIN AND ALASKA THAT iT HAD GONE INTO OR- THE RIVER AND WAS PROMPTLY ARRESTED, SAIGON RADIO SAID.