The Cutting Edge: a Half Century of U.S. Fighter Aircraft R&D
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MS – 204 Charles Lewis Aviation Collection
MS – 204 Charles Lewis Aviation Collection Wright State University Special Collections and Archives Container Listing Sub-collection A: Airplanes Series 1: Evolution of the Airplane Box File Description 1 1 Evolution of Aeroplane I 2 Evolution of Aeroplane II 3 Evolution of Aeroplane III 4 Evolution of Aeroplane IV 5 Evolution of Aeroplane V 6 Evolution of Aeroplane VI 7 Evolution of Aeroplane VII 8 Missing Series 2: Pre-1914 Airplanes Sub-series 1: Drawings 9 Aeroplanes 10 The Aerial Postman – Auckland, New Zealand 11 Aeroplane and Storm 12 Airliner of the Future Sub-series 2: Planes and Pilots 13 Wright Aeroplane at LeMans 14 Wright Aeroplane at Rheims 15 Wilbur Wright at the Controls 16 Wright Aeroplane in Flight 17 Missing 18 Farman Airplane 19 Farman Airplane 20 Antoinette Aeroplane 21 Bleriot and His Monoplane 22 Bleriot Crossing the Channel 23 Bleriot Airplane 24 Cody, Deperdussin, and Hanriot Planes 25 Valentine’s Aeroplane 26 Missing 27 Valentine and His Aeroplane 28 Valentine and His Aeroplane 29 Caudron Biplane 30 BE Biplane 31 Latham Monoplane at Sangette Series 3: World War I Sub-series 1: Aerial Combat (Drawings) Box File Description 1 31a Moraine-Saulnier 31b 94th Aero Squadron – Nieuport 28 – 2nd Lt. Alan F. Winslow 31c Fraser Pigeon 31d Nieuports – Various Models – Probably at Issoudoun, France – Training 31e 94th Aero Squadron – Nieuport – Lt. Douglas Campbell 31f Nieuport 27 - Servicing 31g Nieuport 17 After Hit by Anti-Aircraft 31h 95th Aero Squadron – Nieuport 28 – Raoul Lufbery 32 Duel in the Air 33 Allied Aircraft -
United States Patent (19) 11 Patent Number: 5,836,541 Pham (45) Date of Patent: Nov
USOO5836541A United States Patent (19) 11 Patent Number: 5,836,541 Pham (45) Date of Patent: Nov. 17, 1998 54) EASILY-CONVERTIBLE FIXED-WING 3,986,686 10/1976 Girard ..................................... 244f7 A ROADABLE AIRCRAFT 4,269,374 5/1981 Miller .......................................... 244/2 4,720,061 1/1988 Abdenour et al. ... 244/46 76 Inventor: Roger N. C. Pham, 625 Veranda Ct., 4.881,701 11/1989 Bullard - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 244/2 #1140, Grand Prairie, Tex. 75050 5,050,817 9/1991 Miller .......................................... 244/2 21 Appl.ppl. No.: 859,7329 Primary Examiner-Galen L. Barefoot 57 ABSTRACT 22 Filed: May 21, 1997 57 A fixed-wing four-seat light aircraft that can be easily Related U.S. Application Data converted to a roadway vehicle within minutes by a single perSon in the field, comprising a one-piece wing center panel 63 Continuation-in-part of Ser. No. 811,503, Mar. 5, 1997. with foldable wing tips on each sides. The whole wing unit (51) Int. Cl. ............................................... B64C37.00 is then rotatably mounted on top of the fuselage. The aircraft 52 U.S. CI 24412; 244/46; 244/49 features a conventional front-engine-and-propeller lay-out, 58 Fi la fs - - - - - - - - h - - - - - - - - - - - - - - - - - - - - - - - s 2442. 46.49 with a short fuselage for convenient roadability and 58) Field of Searc 244/135R, 1 R, 100 R. 1 02 R 50 garageability, with horizontal Stabilizer of Significant Span s s s s with foldable tips for adequate flight stability. The vehicle 56) References Cited has a low ride-height with a low center of gravity, four wheels with independent Suspension, nose-height leveling U.S. -
Unclassified Usawc Military Studies Program Paper
UNCLASSIFIED USAWC MILITARY STUDIES PROGRAM PAPER The views expressed in this paper are those of the author and do not necessarily reflect the views of the Department of Defense or any of its agencies. This document may not be released for open pUblication until it has been cleared by the appropriate military service or government agency. THE ROLE OF THE F-117 STEALTH FIGHTER IN SPECIAL OPERATIONS by Lieutenant Colonel Gregory T. Gonyea united States Air Force Dr. Douglas v. J~hnson II Project Advisor A roved for public: DISTRIBUTION STATEMENT A: PP d release~ distribution is unltmlte • U. S. Army War College Carlisle Barracks, Pennsylvania 17013 UNCLASSIFIED 1'" --~OUCEOBY:--N'l"iS.I l u.s. Department of Commerce _0_- l National Technical Information Service r Sprlngrield, Virginia 22161 '-----------~ ABSTRACT AUTHOR: Gregory T. Gonyea, Lt Col, USAF TITLE: The Role of the F-117 Stealth Fighter in special Operations FORMAT: Individual Study Project DATE: 15 April 1993 PAGES: 43 CLASSIFICATION: Unclassified Special operations, as the name implies, are not routine or normal. Neither is the F-117 Stealth Fighter. This paper discusses special operations doctrine, Air Force special operations doctrine, and the applicability of the F-117 to special operations. The capabilities, unit training programs, combat Rerformance, and future developments of the aircraft are used to justify increased integration of the F-117 and special operations communities. The F-117 can offer significant capabilities to the special operations arena. However, many limitations apply. This paper recommends F-117 representation on special operations staff and increased joint exercises to implement F-117 integration in limited special operations activities. -
R/C Model for F3A Competition Biplane
5&PRGHO)RU)$FRPSHWLWLRQ%LSODQH (3)$PRWRU (3 1M23Z06706 Thank you for purchasing Futaba Sky Leaf R/C airplane. To maximize your enjoyment, and to ensure proper flying, please read through this assembly instruction manual. This product is for F3A competition. It can not be assembled or flighted by a beginner. It can be manufactured only for flyers with special skills. )XWDEDJXDUDQWHHVWKLVNLWWREHIUHHIURPGHIHFWVLQERWKPDWHULDODQG ZRUNPDQVKLS DW GDWH RI SXUFKDVH 7KLVZDUUDQW\GRHVQRWFRYHUDQ\ FRPSRQHQW SDUWVGDPDJHGE\XVHRUPRGLrFDWLRQ,QQRFDVHVKDOO)XWDEDOLDELOLW\H[FHHGWKH RULJLQDOFRVWRIWKHSXUFKDVHGNLW)XUWKHU)XWDEDUHVHUYHVWKHULJKWWRFKDQJHRU PRGLI\WKLVZDUUDQW\ZLWKRXWQRWLFH ,Q WKDW )XWDED KDV QR FRQWURO RYHU WKH ILQDO DVVHPEO\ RU PDWHULDO XVHG IRU ILQDO DVVHPEO\QROLDELOLW\VKDOOEHDVVXPHGQRUDFFHSWHGIRUDQ\GDPDJHUHVXOWLQJIURP WKH XVH E\ WKH XVHU RI WKH rQDO XVHUDVVHPEOHG SURGXFW %\ WKH DFW RI XVLQJ WKH XVHUDVVHPEOHGSURGXFWWKHXVHUDFFHSWVDOOUHVXOWLQJOLDELOLW\,IWKHEX\HULVQRW SUHSDUHGWRDFFHSWWKHOLDELOLW\DVVRFLDWHGZLWKWKHSURGXFWWKHEX\HULVDGYLVHGWR UHWXUQWKLVNLWLPPHGLDWHO\LQQHZDQGXQXVHGFRQGLWLRQWRWKHSODFHRISXUFKDVH Precautions ŤƓƓƏƌƆƄƗƌƒƑŃƄƑƇŃƐƒƇƌƲƆƄƗƌƒƑŃƓƕƈƆƄƘƗƌƒƑƖő 1. This product is only designed for use with radio control models. Use of the product described in this instruction manual is limited to radio control models. 2. Modification, adjustment, and parts replacement: Futaba is not responsible for unauthorized modification, adjustment, or replacement of parts on this product. 3. Your Sky Leaf should not be considered a toy, but rather a sophisticated, working model that functions very much like a full- size airplane. Because of its performance capabilities, this airplane, if not assembled and operated correctly, could possibly cause injury to yourself or spectators and damage to property. 4. You must assemble the model according to the instructions. Do not alter or modify the model, as doing so may result in an unsafe or unflyable model. In a few cases the instructions may differ slightly from the figures. -
Air Force Next-Generation Bomber: Background and Issues for Congress
Air Force Next-Generation Bomber: Background and Issues for Congress Jeremiah Gertler Specialist in Military Aviation December 22, 2009 Congressional Research Service 7-5700 www.crs.gov RL34406 CRS Report for Congress Prepared for Members and Committees of Congress Air Force Next-Generation Bomber: Background and Issues for Congress Summary As part of its proposed FY2010 defense budget, the Administration proposed deferring the start of a program to develop a next-generation bomber (NGB) for the Air Force, pending the completion of the 2010 Quadrennial Defense Review (QDR) and associated Nuclear Posture Review (NPR), and in light of strategic arms control negotiations with Russia. The Administration’s proposed FY2010 budget requested no funding specifically identified in public budget documents as being for an NGB program. Prior to the submission of the FY2010 budget, the Air Force was conducting research and development work aimed at fielding a next-generation bomber by 2018. Although the proposed FY2010 defense budget proposed deferring the start of an NGB program, the Secretary of Defense and Air Force officials in 2009 have expressed support for the need to eventually start such a program. The Air Force’s FY2010 unfunded requirements list (URL)—a list of programs desired by the Air Force but not funded in the Air Force’s proposed FY2010 budget—includes a classified $140-million item that some press accounts have identified as being for continued work on a next-generation bomber. FY2010 defense authorization bill: The conference report (H.Rept. 111-288 of October 7, 2009) on the FY2010 defense authorization act (H.R. -
1 17A Stealth Fighter Organizations
HISTORY AND LINEAGE OF THE F- 1 17A STEALTH FIGHTER ORGANIZATIONS DECEMBER 1991 SPECIAL STUDY HO-91-2 OFFICE OF HIST RY HEADQUARTERS, 37TH FPGHTER WING TWELFTH AIR FORCE TACTICAL AIR COMMAND INTRODUCTION In 1978, the Air Force awarded a full-scale development contract for the F-117A Stealth Fighter to Lockheed Corporation's Advanced Development Projects (the famous Skunk Works). Thirty- one months later, on 18 June 1981, the F-117A made its first flight. Meanwhile, the Tactical Air Command (TAC) decided to set up a group-level organization to guide the F-117A to an initial operating capability. That organization became the 4450th Tactical Group (TG), which officially activated on 15 October 1979 at Nellis AFB, Nevada. The 4450 TG began flying operations in 1981 from the Tonopah Test Range Airfield, located approximately 130 miles northwest of Las Vegas, Nevada. Lockheed test pilots put the Stealth Fighter through its early paces. The 4450 TG also operated the A-7D as a surrogate trainer for the F-l17A, and these operations continued until 15 October 1982 under the guise of an avionics test mis- sion. October 15th is important to the program because on that date Maj Alton C. Whitley, Jr. became the first 4450 TG pilot to fly the F-117A. The 4450 TG then achieved an initial operating capability with the F-117A in October 1983. The 4450 TG's mission continued to evolve under a cloak of secrecy--all Tonopah training flights conducted at night under the cover of darkness--until late 1988. On 10 November 1988, the Air Force brought the F-117A from behind a "black veil" by publicly acknowledging its existence. -
A52 Mosquito Light Bomber
A52 Mosquito Light Bomber The de Havilland DH 98 Mosquito was one of the greatest combat Initial delays in production were due to the difficulties of importing aircraft of World War II. Originally conceived as a fast, unarmed, light engines, tools and priority equipment from de Havilland in Great Britain bomber that would be able to outfly fighters, the lightweight, all-wood and Canada. Soon after production began, the manufacturer discovered construction “Mossie” first flew on Nov. 25, 1940, and had a top speed an issue with wing assembly, and the first 50 sets of wings required of almost 400 mph. Mosquitoes were built in several different versions, modification. This, and the discovery of flutter issues, further delayed including fighter-bombers (FBs), photo-reconnaissance, day and night production, which eventually amounted to just 75 airplanes being built bombers, and long-range day and night fighters. between March 1944 and May 1945. By the end of the war, production issues had been resolved, and 212 Mosquitoes were built at Bankstown. Mosquitoes were assembled in Great Britain, Canada, and in 1942, the Of these, six FB Mk 40s were converted for photo reconnaissance as Australian de Havilland factory at Bankstown commenced production of PR Mk 40s, and a further 28 were converted to PR Mk 41s, with the last an FB version of the Mosquito. A Royal Air Force Mk II (DD664) was delivered July 22, 1948. delivered to Bankstown and used as a prototype for the Australian FB Mk 40s. It made its first flight on Dec. 17, 1942, and was later delivered In addition to the Australian-built Mosquitoes, 76 British-built Mosquitoes to the Royal Australian Air Force (RAAF) on Jan. -
Artifacts and Aircraft
International Journal of Business, Humanities and Technology Vol. 5, No. 2; April 2015 The Ancients: Artifacts and Aircraft Susan Kelly Archer, EdD Embry-Riddle Aeronautical University Department of Doctoral Studies College of Aviation Daytona Beach, Florida USA Abstract Throughout literature and other art forms, certain themes appear repeatedly. The same might be said for engineering designs, specifically the design of aerospace vehicles. In 1996, Lumir Janku wrote about a set of artifacts, discovered in Peru and determined to be Pre-Columbian, that can be interpreted as models of delta- winged fliers. The design of the Peruvian artifacts has been interpreted in multiple ways by a variety of professionals. The delta wing was also incorporated into the design of civilian aircraft during the 20th Century. Modern delta-winged aircraft were used successfully in both military and civilian applications for more than 40 years. It is interesting to read about the possibility that this aeronautical design may have originated millennia earlier with a culture that did not leave written records to explain its artifacts crafted in gold. Keywords: aviation history, delta wing, Pre-Columbian artifacts Throughout literature and other art forms, certain themes appear repeatedly. The same might be said for engineering designs, specifically the design of aerospace vehicles. Man’s fascination with how birds fly can be linked to the ancient legends of Daedalus or the winged Egyptian gods, and then more recently to John Damien’s attempt to fly with wings made from chicken feathers (Brady, 2000) or Otto Lillienthal’s essays linking the physiology of birds to the design of early gliders (Lillienthal, 2001). -
04 Delta Wings
ExperimentalExperimental AerodynamicsAerodynamics Lecture 4: Delta wing experiments G. Dimitriadis Experimental Aerodynamics Introduction •! In this course we will demonstrate the use of several different experimental aerodynamic methodologies •! The particular application will be the aerodynamics of Delta wings at low airspeeds. •! Delta wings are of particular interest because of their lift generation mechanism. Experimental Aerodynamics Delta wing history •! Until the 1930s the vast majority of aircraft featured rectangular, trapezoidal or elliptical wings. •! Delta wings started being studied in the 1930s by Alexander Lippisch in Germany. •! Lippisch wanted to create tail-less aircraft, and Delta wings were one of the solutions he proposed. Experimental Aerodynamics Delta Lippisch DM-1 Designed as an interceptor jet but never produced. The photos show a glider prototype version. Experimental Aerodynamics High speed flight •! After the war, the potential of Delta wings for supersonic flight was recognized both in the US and the USSR. MiG-21 Convair XF-92 Experimental Aerodynamics Low speed performance •! Although Delta wings are designed for high speeds, they still have to take off and land at small airspeeds. •! It is important to determine the aerodynamic forces acting on Delta wings at low speed. •! The lift generated by such wings are low speeds can be split into two contributions: –! Potential flow lift –! Vortex lift Experimental Aerodynamics Delta wing geometry cb Wing surface: S = 2 2b Aspect ratio: AR = "! c c! b AR Sweep angle: tan ! = = 2c 4 b/2! Experimental Aerodynamics Potential flow lift •! Slender wing theory •! The wind is discretized into transverse segments. •! The flow around each segment is modeled as a 2D flow past a flat plate perpendicular to the free stream Experimental Aerodynamics Slender wing theory •! The problem of calculating the flow around the wing becomes equivalent to calculating the flow around each 2D segment. -
Lightweight Fighter Aircraft Program
/ C '3 3 'GOVERNMENT Senate Hearing^ Storage Before the Committee on Appro priation s Y)t )C U M r HTS -------- -------------- L ig h tw e ig h t F ig h te r A ir c ra ft P ro g ra m . T 0 7 6 MAY 1 ? 1975 t h ^ ta« un^ X s,ty KANSA o Lightweight Fighter Aircraft Program m in H < —'— J- □ " 1 □ IT Fis ca l Y ear 1976 H H < 94“ CONGRESS, FIRST SESSION LIGHTWEIGHT FIGH TER AIRC RA FT PROGRAM H E A R IN G BEFORE A SUBCOMMITTEE OF THE COMMITTEE ON APPROPRIATIONS UNITED STATES SENATE NIN ETY-F OURTH CONGRESS F IR ST SE SS IO N Printed for the use of the Committee on Appropriations U.S. GOVERNMENT PRINTING OFFICE 52-600 0 WASHINGTON : 1975 SU BC OM MITTE E OF THE CO MMIT TE E ON APP ROPR IA TIO NS JO HN L. McC LE LL AN , A rk an sa s, C hair m an JO HN C. ST EN NIS , Mississ ippi MILTO N R. YOUNG, Nor th Dak ot a JO HN O. PA ST OR E, Rhode Island ROMAN L. HR US KA , Neb ra sk a WA RREN G. MAGNUSON, W as hing ton CL IF FO RD I’. CA SE, New Je rs ey MIK E MANS FIEL D, M on tana HIRA M L. FON G, Haw aii GALE W. Mc GE E, Wyomi ng TE D ST EV EN S, Alaska WILL IAM I’ROX MIRE, Wisco nsin RICH AR D S. -
F—18 Navy Air Combat Fighter
74 /2 >Af ^y - Senate H e a r tn ^ f^ n 12]$ Before the Committee on Appro priations (,() \ ER WIIA Storage ime nts F EB 1 2 « T H e -,M<rUN‘U«sni KAN S A S S F—18 Na vy Air Com bat Fighter Fiscal Year 1976 th CONGRESS, FIRS T SES SION H .R . 986 1 SPECIAL HEARING F - 1 8 NA VY AIR CO MBA T FIG H TER HEARING BEFORE A SUBC OMMITTEE OF THE COMMITTEE ON APPROPRIATIONS UNITED STATES SENATE NIN ETY-FOURTH CONGRESS FIR ST SE SS IO N ON H .R . 9 8 6 1 AN ACT MAKIN G APP ROPR IA TIO NS FO R THE DEP ARTM EN T OF D EFEN SE FO R T H E FI SC AL YEA R EN DI NG JU N E 30, 1976, AND TH E PE RIO D BE GIN NIN G JU LY 1, 1976, AN D EN DI NG SEPT EM BER 30, 1976, AND FO R OTH ER PU RP OSE S P ri nte d fo r th e use of th e Com mittee on App ro pr ia tio ns SPECIAL HEARING U.S. GOVERNM ENT PRINT ING OFF ICE 60-913 O WASHINGTON : 1976 SUBCOMMITTEE OF THE COMMITTEE ON APPROPRIATIONS JOHN L. MCCLELLAN, Ark ans as, Chairman JOH N C. ST ENN IS, Mississippi MILTON R. YOUNG, No rth D ako ta JOH N O. P ASTORE, Rhode Island ROMAN L. HRUSKA, N ebraska WARREN G. MAGNUSON, Washin gton CLIFFORD I’. CASE, New Je rse y MIK E MANSFIEL D, Montana HIRAM L. -
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Memorial Tributes: Volume 8 BEN RICH 200 Copyright National Academy of Sciences. All rights reserved. Memorial Tributes: Volume 8 BEN RICH 201 Ben Rich 1925-1995 By Willis M. Hawkins Ben Rich died on January 5, 1995, after a full career as an engineer, a designer, and an effective and cherished executive. I first knew Ben when he joined the Lockheed Aircraft Company in Burbank back in 1950. He came to us from the University of California, Berkeley, and University of California, Los Angeles, with a master's degree in mechanical engineering. At the time, I was in charge of the Advanced Design Organization under the Deputy Chief Engineer C. L. "Kelly" Johnson, and we were working on our first Mach 2+ Air Force fighter proposal, which became the F-104. Ben was assigned the task of analyzing the aerothermodynamic performance of the power plant with little or no existing state of the art for supersonic inlets. It is a testament to Ben's understanding of this specialty that the inlet configuration was classified by the Air Force and the details obscured in Air Force-released pictures of the airplane for a number of years. The Lockheed "Skunk Works," which had originated during the design and development of the original P-80 prototype "Lulu-Belle," was being reactivated at about the time that the F-104 was conceived. Its specific purpose was the secret development of the U-2, and Ben was ''borrowed" by Kelly Johnson to help on that program. His "temporary'' assignment became his career. Under Kelly, Ben pursued his specialty of aerothermodynamic analysis.