Aerospace Micro-Lesson
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Aerodynamics Material - Taylor & Francis
CopyrightAerodynamics material - Taylor & Francis ______________________________________________________________________ 257 Aerodynamics Symbol List Symbol Definition Units a speed of sound ⁄ a speed of sound at sea level ⁄ A area aspect ratio ‐‐‐‐‐‐‐‐ b wing span c chord length c Copyrightmean aerodynamic material chord- Taylor & Francis specific heat at constant pressure of air · root chord tip chord specific heat at constant volume of air · / quarter chord total drag coefficient ‐‐‐‐‐‐‐‐ , induced drag coefficient ‐‐‐‐‐‐‐‐ , parasite drag coefficient ‐‐‐‐‐‐‐‐ , wave drag coefficient ‐‐‐‐‐‐‐‐ local skin friction coefficient ‐‐‐‐‐‐‐‐ lift coefficient ‐‐‐‐‐‐‐‐ , compressible lift coefficient ‐‐‐‐‐‐‐‐ compressible moment ‐‐‐‐‐‐‐‐ , coefficient , pitching moment coefficient ‐‐‐‐‐‐‐‐ , rolling moment coefficient ‐‐‐‐‐‐‐‐ , yawing moment coefficient ‐‐‐‐‐‐‐‐ ______________________________________________________________________ 258 Aerodynamics Aerodynamics Symbol List (cont.) Symbol Definition Units pressure coefficient ‐‐‐‐‐‐‐‐ compressible pressure ‐‐‐‐‐‐‐‐ , coefficient , critical pressure coefficient ‐‐‐‐‐‐‐‐ , supersonic pressure coefficient ‐‐‐‐‐‐‐‐ D total drag induced drag Copyright material - Taylor & Francis parasite drag e span efficiency factor ‐‐‐‐‐‐‐‐ L lift pitching moment · rolling moment · yawing moment · M mach number ‐‐‐‐‐‐‐‐ critical mach number ‐‐‐‐‐‐‐‐ free stream mach number ‐‐‐‐‐‐‐‐ P static pressure ⁄ total pressure ⁄ free stream pressure ⁄ q dynamic pressure ⁄ R -
Memorandum Board of Supervisors
MEMORANDUM OFFICE OF THE BOARD OF SUPERVISORS COUNTY OF PLACER TO: Honorable Board of Supervisors FROM: Jennifer Montgomery Supervisor, District 5 DATE: October 9,2012 SUBJECT: RESOLUTION - Adopt and present a Resolution to Clarence Emil "Bud" Anderson for his outstanding service to his country and his community. ACTION REQUESTED Adopt and present a Resolution to Clarence Emil "Bud" Anderson for his outstanding service to his country and his community. BACKGROUND Colonel Anderson has over thirty years of military service, and was a test pilot at Wright Field where he also served as Chief of Fighter Operations. He also served at Edwards Air Force Base where he was Chief of Flight Test Operations and Deputy Director of Flight Test. Colonel Anderson served two tours at The Pentagon and commanded three fighter organizations. From June to December 1970, he commanded the 355th Tactical Fighter Wing, an F-105 Thunderchief unit, during its final months of service in the Vietnam War, and retired in March 1972. He was decorated twenty-five times for his service to the United States. After his retirement from active duty as a Colonel, he became the manager of the McDonnell Aircraft Company's Flight Test Facility at Edwards AFB, serving there until 1998. During his career, he flew over 100 types of aircraft, and logged over 7,000 hours. Anderson is possibly best known for his close friendship with General Chuck Yeager from World War II, where both served in the 35th Fighter Group, to the present. Yeager once called him "The best fighter pilot I ever saw". -
“Bob” Hoover IAC’S 2009 Hall of Fame Inductee
JANUARY 2010 OFFICIALOFFICIAL MAGAZINEMAGAZINE OFOF TTHEHE INTERNATIONALI AEROBATIC CLUB R.A. “Bob” Hoover IAC’s 2009 Hall of Fame Inductee • The IAC turns 40 • The Doug Yost Scholarship PLATINUM SPONSORS Northwest Insurance Group/Berkley Aviation Sherman Chamber of Commerce GOLD SPONSORS Aviat Aircraft Inc. The IAC wishes to thank Denison Chamber of Commerce MT Propeller GmbH the individual and MX Aircraft corporate sponsors Southeast Aero Services/Extra Aircraft of the SILVER SPONSORS David and Martha Martin 2009 National Aerobatic Jim Kimball Enterprises Norm DeWitt Championships. Rhodes Real Estate Vaughn Electric BRONZE SPONSORS ASL Camguard Bill Marcellus Digital Solutions IAC Chapter 3 IAC Chapter 19 IAC Chapter 52 Lake Texoma Jet Center Lee Olmstead Andy Olmstead Joe Rushing Mike Plyler Texoma Living! Magazine Laurie Zaleski JANUARY 2010 • VOLUME 39 • NUMBER 1 • IAC SPORT AEROBATICS CONTENTS FEATURES 6 R.A. “Bob” Hoover IAC’s 2009 Hall of Fame Inductee – Reggie Paulk 14 Training Notes Doug Yost Scholarship – Lise Lemeland 18 40 Years Ago . The IAC comes to life – Phil Norton COLUMNS 6 3 President’s Page – Doug Bartlett 28 Just for Starters – Greg Koontz 32 Safety Corner – Stan Burks DEPARTMENTS 14 2 Letter from the Editor 4 Newsbriefs 30 IAC Merchandise 31 Fly Mart & Classifieds THE COVER IAC Hall of Famer R. A. “Bob” Hoover at the controls of his Shrike Commander. 18 – Photo: EAA Photo Archives LETTER from the EDITOR OFFICIAL MAGAZINE OF THE INTERNATIONAL AEROBATIC CLUB Publisher: Doug Bartlett by Reggie Paulk IAC Manager: Trish Deimer Editor: Reggie Paulk Senior Art Director: Phil Norton Interim Dir. of Publications: Mary Jones Copy Editor: Colleen Walsh Contributing Authors: Doug Bartlett Lise Lemeland Stan Burks Phil Norton Greg Koontz Reggie Paulk IAC Correspondence International Aerobatic Club, P.O. -
“One of the World's Best Air Shows” Coming to Goldsboro, NC Seymour
For Immediate Release “One of the world’s best air shows” coming to Goldsboro, NC USAF Thunderbirds – Courtesy Staff Sgt Richard Rose Jr. Seymour Johnson AFB – Goldsboro, NC – “Wings Over Wayne is one of the world’s best air shows,” said Chuck Allen, Mayor of Goldsboro. “Seymour Johnson does a phenomenal job attracting the best lineup of airpower and performers, alongside the F-15E Strike Eagle and KC-135 aircraft already stationed at the base.” Located in Goldsboro, the seat of Wayne County, Seymour Johnson Air Force Base will stage and choreograph the Wings Over Wayne Air Show on Saturday and Sunday, April 27-28. Headlining the exhibition from Nellis Air Force Base in Nevada, is the premier Air Force jet demonstration team, the Thunderbirds. The gates open each day at 9 AM, with aerial displays from 11 AM until 4:30 PM. “As our guests, you will be able to see world-class acrobatics and ground demonstrations that are truly a sight to be seen,” said Colonel Donn Yates, Commander of Seymour Johnson’s 4thFighter Wing. “Some of the performers scheduled include the F- 35 Demonstration Team, Tora! Tora! Tora!, the US Army Black Daggers, the B-2 Spirit, and other elite aircraft within the Air Force Arsenal.” Wings Over Wayne is a family-friendly expo including the Kids’ Zone, occupying one of the largest aircraft hangars on the base. A $10 admission charge covers access to the Zone for the entire day. “There is something for everyone,” said Colonel Yates. “Come out and witness this spectacular show while enjoying great food and fun with your family and ours.” “For the more serious air show enthusiasts, the two-day show has evolved into an air show week,” said Mayor Allen. -
Brazilian 14-Xs Hypersonic Unpowered Scramjet Aerospace Vehicle
ISSN 2176-5480 22nd International Congress of Mechanical Engineering (COBEM 2013) November 3-7, 2013, Ribeirão Preto, SP, Brazil Copyright © 2013 by ABCM BRAZILIAN 14-X S HYPERSONIC UNPOWERED SCRAMJET AEROSPACE VEHICLE STRUCTURAL ANALYSIS AT MACH NUMBER 7 Álvaro Francisco Santos Pivetta Universidade do Vale do Paraíba/UNIVAP, Campus Urbanova Av. Shishima Hifumi, no 2911 Urbanova CEP. 12244-000 São José dos Campos, SP - Brasil [email protected] David Romanelli Pinto ETEP Faculdades, Av. Barão do Rio Branco, no 882 Jardim Esplanada CEP. 12.242-800 São José dos Campos, SP, Brasil [email protected] Giannino Ponchio Camillo Instituto de Estudos Avançados/IEAv - Trevo Coronel Aviador José Alberto Albano do Amarante, nº1 Putim CEP. 12.228-001 São José dos Campos, SP - Brasil. [email protected] Felipe Jean da Costa Instituto Tecnológico de Aeronáutica/ITA - Praça Marechal Eduardo Gomes, nº 50 Vila das Acácias CEP. 12.228-900 São José dos Campos, SP - Brasil [email protected] Paulo Gilberto de Paula Toro Instituto de Estudos Avançados/IEAv - Trevo Coronel Aviador José Alberto Albano do Amarante, nº1 Putim CEP. 12.228-001 São José dos Campos, SP - Brasil. [email protected] Abstract. The Brazilian VHA 14-X S is a technological demonstrator of a hypersonic airbreathing propulsion system based on supersonic combustion (scramjet) to fly at Earth’s atmosphere at 30km altitude at Mach number 7, designed at the Prof. Henry T. Nagamatsu Laboratory of Aerothermodynamics and Hypersonics, at the Institute for Advanced Studies. Basically, scramjet is a fully integrated airbreathing aeronautical engine that uses the oblique/conical shock waves generated during the hypersonic flight, to promote compression and deceleration of freestream atmospheric air at the inlet of the scramjet. -
HISTORICAL PERSPECTIVE a Need for Speed
n HISTORICAL PERSPECTIVE A need for speed Mach 0.8 to 1.2 and above the speed of powerful turbine engine available. To mit- Skystreak taught lots sound, respectively). The U.S. Army Air igate as much risk as possible, the team Forces took responsibility for supersonic kept the design simple, using a conven- about flight near research—which resulted in Chuck Yea- tional straight wing rather than the new ger breaking the sound barrier in the Bell and mostly unproven swept wing. The the sound barrier X-1 on Oct. 14, 1947. That historic event 5,000-lb.-thrust (22-kilonewton) Allison overshadowed the highly successful re- J35-A-11 engine filled the fuselage, leav- BY MICHAEL LOmbARDI search conducted by the pilots who flew ing just enough room to house instrumen- s World War II was coming to a the Douglas D-558-1 Skystreak to the edge tation and a pilot in a cramped cockpit. close, advances in high-speed aero- of the sound barrier while capturing new Because of the lack of knowledge about Adynamics were rapidly progressing world speed records. the survivability of a high-altitude, high- beyond the ability of the wind tunnels of The D-558-1 was developed by the speed bailout, Douglas engineers designed the day, prompting a dramatic expansion Douglas Aircraft Company, today a part a jettisonable nose section that could pro- of flight-test research and experimental of Boeing, at its El Segundo (Calif.) tect the pilot until a safe bailout speed was aircraft. Division. It was designed by a team led reached. -
Drag Bookkeeping
Drag Drag Bookkeeping Drag may be divided into components in several ways: To highlight the change in drag with lift: Drag = Zero-Lift Drag + Lift-Dependent Drag + Compressibility Drag To emphasize the physical origins of the drag components: Drag = Skin Friction Drag + Viscous Pressure Drag + Inviscid (Vortex) Drag + Wave Drag The latter decomposition is stressed in these notes. There is sometimes some confusion in the terminology since several effects contribute to each of these terms. The definitions used here are as follows: Compressibility drag is the increment in drag associated with increases in Mach number from some reference condition. Generally, the reference condition is taken to be M = 0.5 since the effects of compressibility are known to be small here at typical conditions. Thus, compressibility drag contains a component at zero-lift and a lift-dependent component but includes only the increments due to Mach number (CL and Re are assumed to be constant.) Zero-lift drag is the drag at M=0.5 and CL = 0. It consists of several components, discussed on the following pages. These include viscous skin friction, vortex drag due to twist, added drag due to fuselage upsweep, control surface gaps, nacelle base drag, and miscellaneous items. The Lift-Dependent drag, sometimes called induced drag, includes the usual lift- dependent vortex drag together with lift-dependent components of skin friction and pressure drag. For the second method: Skin Friction drag arises from the shearing stresses at the surface of a body due to viscosity. It accounts for most of the drag of a transport aircraft in cruise. -
Max Neuhaus, R. Murray Schafer, and the Challenges of Noise
University of Kentucky UKnowledge Theses and Dissertations--Music Music 2018 MAX NEUHAUS, R. MURRAY SCHAFER, AND THE CHALLENGES OF NOISE Megan Elizabeth Murph University of Kentucky, [email protected] Digital Object Identifier: https://doi.org/10.13023/etd.2018.233 Right click to open a feedback form in a new tab to let us know how this document benefits ou.y Recommended Citation Murph, Megan Elizabeth, "MAX NEUHAUS, R. MURRAY SCHAFER, AND THE CHALLENGES OF NOISE" (2018). Theses and Dissertations--Music. 118. https://uknowledge.uky.edu/music_etds/118 This Doctoral Dissertation is brought to you for free and open access by the Music at UKnowledge. It has been accepted for inclusion in Theses and Dissertations--Music by an authorized administrator of UKnowledge. For more information, please contact [email protected]. STUDENT AGREEMENT: I represent that my thesis or dissertation and abstract are my original work. Proper attribution has been given to all outside sources. I understand that I am solely responsible for obtaining any needed copyright permissions. I have obtained needed written permission statement(s) from the owner(s) of each third-party copyrighted matter to be included in my work, allowing electronic distribution (if such use is not permitted by the fair use doctrine) which will be submitted to UKnowledge as Additional File. I hereby grant to The University of Kentucky and its agents the irrevocable, non-exclusive, and royalty-free license to archive and make accessible my work in whole or in part in all forms of media, now or hereafter known. I agree that the document mentioned above may be made available immediately for worldwide access unless an embargo applies. -
Fluid Mechanics, Drag Reduction and Advanced Configuration Aeronautics
NASA/TM-2000-210646 Fluid Mechanics, Drag Reduction and Advanced Configuration Aeronautics Dennis M. Bushnell Langley Research Center, Hampton, Virginia December 2000 The NASA STI Program Office ... in Profile Since its founding, NASA has been dedicated to CONFERENCE PUBLICATION. Collected the advancement of aeronautics and space papers from scientific and technical science. The NASA Scientific and Technical conferences, symposia, seminars, or other Information (STI) Program Office plays a key meetings sponsored or co-sponsored by part in helping NASA maintain this important NASA. role. SPECIAL PUBLICATION. Scientific, The NASA STI Program Office is operated by technical, or historical information from Langley Research Center, the lead center for NASA programs, projects, and missions, NASA's scientific and technical information. The often concerned with subjects having NASA STI Program Office provides access to the substantial public interest. NASA STI Database, the largest collection of aeronautical and space science STI in the world. TECHNICAL TRANSLATION. English- The Program Office is also NASA's institutional language translations of foreign scientific mechanism for disseminating the results of its and technical material pertinent to NASA's research and development activities. These mission. results are published by NASA in the NASA STI Report Series, which includes the following Specialized services that complement the STI report types: Program Office's diverse offerings include creating custom thesauri, building customized TECHNICAL PUBLICATION. Reports of databases, organizing and publishing research completed research or a major significant results ... even providing videos. phase of research that present the results of NASA programs and include extensive For more information about the NASA STI data or theoretical analysis. -
Airspace: Seeing Sound Grades
National Aeronautics and Space Administration GRADES K-8 Seeing Sound airspace Aeronautics Research Mission Directorate Museum in a BO SerieXs www.nasa.gov MUSEUM IN A BOX Materials: Seeing Sound In the Box Lesson Overview PVC pipe coupling Large balloon In this lesson, students will use a beam of laser light Duct tape to display a waveform against a flat surface. In doing Super Glue so, they will effectively“see” sound and gain a better understanding of how different frequencies create Mirror squares different sounds. Laser pointer Tripod Tuning fork Objectives Tuning fork activator Students will: 1. Observe the vibrations necessary to create sound. Provided by User Scissors GRADES K-8 Time Requirements: 30 minutes airspace 2 Background The Science of Sound Sound is something most of us take for granted and rarely do we consider the physics involved. It can come from many sources – a voice, machinery, musical instruments, computers – but all are transmitted the same way; through vibration. In the most basic sense, when a sound is created it causes the molecule nearest the source to vibrate. As this molecule is touching another molecule it causes that molecule to vibrate too. This continues, from molecule to molecule, passing the energy on as it goes. This is also why at a rock concert, or even being near a car with a large subwoofer, you can feel the bass notes vibrating inside you. The molecules of your body are vibrating, allowing you to physically feel the music. MUSEUM IN A BOX As with any energy transfer, each time a molecule vibrates or causes another molecule to vibrate, a little energy is lost along the way, which is why sound gets quieter with distance (Fig 1.) and why louder sounds, which cause the molecules to vibrate more, travel farther. -
PRESS RELEASE – Chuck Yeager
FOR IMMEDIATE RELEASE PRESS RELEASE YEAGER AIRPORT MOURNS PASSING OF GENERAL CHUCK YEAGER Yeager Airport Staff and the Central West Virginia Regional Airport Board Members are mourning the loss of Brig. Gen. Charles “Chuck” Yeager today. His bravery and dedication will be remembered around the world for generations to come. “Gen. Yeager is a true pioneer in the world of aviation,” said Yeager Airport Director and CEO NicK Keller. “It is rare to be the first to ever do something, and Gen. Yeager did that by breaking the sound barrier and putting our great country ahead of its time in aviation.” General Yeager got his start as a pilot in 1941 when he signed for the Army Air Corps, now Known as the U.S. Air Force. Yeager’s military career spanned six decades and four wars. During World War II, Gen. Yeager flew 64 missions and shot down 13 German planes. Yeager’s plane was shot down over France in 1944 but he escaped capture. After the war, in true West Virginia fashion, Yeager continued serving his country as a flight instructor and test pilot at Wright Field in Ohio. It was there that his exceptional sKills were quicKly recognized, and he was chosen to be the first to fly the rocKet-powered Bell X-1. “General Yeager exemplified everything it means to be a West Virginian”, said Central West Virginia Regional Airport Authority Board Chairman Ed Hill. “Born and raised in Lincoln County, General Yeager’s hard work, dedication, skill, and bravery defined his historic career. Our entire Board is saddened by the loss of a fellow West Virginian, and a leader in aviation.” Yeager made history in 1947, when his Bell X-1 broke the speed of sound over a lake in Southern California. -
Call No. 310 Contract Id. 111037 Jefferson County
eProposal Jan-2009 CALL NO. 310 CONTRACT ID. 111037 JEFFERSON COUNTY FED/STATE PROJECT NUMBER JL03 056 0264 014-016 DESCRIPTION WATTERSON EXPRESSWAY (I-264) WORK TYPE SOUND BARRIER WALL PRIMARY COMPLETION DATE 6/30/2012 LETTING DATE: August 19, 2011 Sealed Bids will be received electronically through the Bid Express bidding service until 10:00 AM EASTERN DAYLIGHT TIME August 19, 2011. Bids will be publicly announced at 10:00 AM EASTERN DAYLIGHT TIME. ROAD PLANS REQUIRED BID PROPOSAL GUARANTY: Not less than 5% of the total bid. JEFFERSON COUNTY Contract ID: 111037 JL03 056 0264 014-016 Page 2 of 103 TABLE OF CONTENTS PART I SCOPE OF WORK · PROJECT(S), COMPLETION DATE(S), & LIQUIDATED DAMAGES · CONTRACT NOTES · STATE CONTRACT NOTES · NATIONAL HIGHWAY · DGA BASE · DGA BASE FOR SHOULDERS · SPECIAL NOTE(S) APPLICABLE TO PROJECT · RIGHT OF WAY NOTES · UTILITY CLEARANCE · KPDES STORM WATER PERMIT, BMP AND NOI · COMMUNICATING ALL PROMISES PART II SPECIFICATIONS AND STANDARD DRAWINGS · SPECIFICATIONS REFERENCE · SUPPLEMENTAL SPECIFICATIONS PART III EMPLOYMENT, WAGE AND RECORD REQUIREMENTS · LABOR AND WAGE REQUIREMENTS · EXECUTIVE BRANCH CODE OF ETHICS · KENTUCKY EQUAL EMPLOYMENT OPPORTUNITY ACT OF 1978 · PROJECT WAGE RATES PART IV INSURANCE PART V BID ITEMS JEFFERSON COUNTY Contract ID: 111037 JL03 056 0264 014-016 Page 3 of 103 PART I SCOPE OF WORK JEFFERSON COUNTY Contract ID: 111037 JL03 056 0264 014-016 Page 4 of 103 CONTRACT ID - 111037 ADMINISTRATIVE DISTRICT - 05 PROJECT(S) IDENTIFICATION AND DESCRIPTION: COUNTY - JEFFERSON PCN - DE05602641137 JL03 056 0264 014-016 WATTERSON EXPRESSWAY (I-264) INSTALL SOUND BARRIER WALL BETWEEN THE NEWBURG ROAD EXIT RAMP AND THE BARDSTOWN ROAD ENTRANCE RAMP.