Constraints for STOL Operations in South Florida Conurbation Cedric Y
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
A Design Study Me T Rop"Ol Itan Air Transit System
NASA CR 73362 A DESIGN STUDY OF A MET R OP"OL ITAN AIR TRANSIT SYSTEM MAT ir 0 ± 0 49 PREPARED UNDER, NASA-ASEE SUMMER FACULTY FELLOWSHIP PROGRAM ,IN Cq ENGINEERING SYSTEMS DESIGN NASA CONTRACT NSR 05-020-151 p STANFORD UNIVERSITY STANFORD CALIFORNIA CL ceoroducedEAR'C-by thEGHOU AUGUST 1969 for Federal Scientific &Va Tec1nical 2 Information Springfied NASA CR 73362 A DESIGN STUDY OF A METROPOLITAN AIR TRANSIT SYSTEM MAT Prepared under NASA Contract NSR 05-020-151 under the NASA-ASEE Summer Faculty Fellowship Program in Engineering Systems Design, 16 June 29 August, 1969. Faculty Fellows Richard X. Andres ........... ......... ..Parks College Roger R. Bate ....... ...... .."... Air Force Academy Clarence A. Bell ....... ......"Kansas State University Paul D. Cribbins .. .... "North Carolina State University William J. Crochetiere .... .. ........ .Tufts University Charles P. Davis . ... California State Polytechnic College J. Gordon Davis . .... Georgia Institute of Technology Curtis W. Dodd ..... ....... .Southern Illinois University Floyd W. Harris .... ....... .... Kansas State University George G. Hespelt ........ ......... .University of Idaho Ronald P. Jetton ...... ............ .Bradley University Kenneth L. Johnson... .. Milwaukee School of Engineering Marshall H. Kaplan ..... .... Pennsylvania State University Roger A. Keech . .... California State Polytechnic College Richard D. Klafter... .. .. Drexel Institute of Technology Richard S. Marleau ....... ..... .University of Wisconsin Robert W. McLaren ..... ....... University'of Missouri James C. Wambold..... .. Pefinsylvania State University Robert E. Wilson..... ..... Oregon State University •Co-Directors Willi'am Bollay ...... .......... Stanford University John V. Foster ...... ........... .Ames Research Center Program Advisors Alfred E. Andreoli . California State Polytechnic College Dean F. Babcock .... ........ Stanford Research Institute SUDAAR NO. 387 September, 1969 i NOT FILMED. ppECEDING PAGE BLANK CONTENTS Page CHAPTER 1--INTRODUCTION ... -
ICAO Safety Report |2020
SAFETY Safety Report 2020 Edition Foreword A Coordinated, Risk-based Approach to Improving Global Aviation Safety The air transport industry plays a major role in global economic activity and development. One of the key elements to maintaining the vitality of civil aviation is to ensure safe, secure, efficient and environmentally sustainable operations at the global, regional and national levels. A specialized agency of the United Nations, the International Civil Aviation Organization (ICAO) was established in 1944 to promote the safe and orderly development of international civil aviation throughout the world. ICAO promulgates Standards and Recommended Practices (SARPs) to facilitate harmonized regulations in aviation safety, security, efficiency and environmental protection on a global basis. Today, ICAO manages over 12 000 SARPs across the 19 Annexes and five Procedures for Air Navigation Services (PANS) to the Convention on International Civil Aviation (Chicago Convention), many of which are constantly evolving in tandem with latest developments and innovations. ICAO serves as the primary forum for co-operation in all fields of civil aviation among its 193 Member States. Improving the safety of the global air transport system is ICAO’s guiding and most fundamental strategic objective. The Organization works constantly to address and enhance global aviation safety through the following coordinated activities: • Policy and Standardization; • Monitoring of key safety trends and indicators; • Safety Analysis; and • Implementing programmes to address safety issues. The ICAO Global Aviation Safety Plan (GASP) presents the strategy in support of the prioritization and continuous improvement of aviation safety. The GASP sets the goals and targets and outlines key safety enhancement initiatives (SEIs) aimed at improving safety at the international, regional and national levels. -
Lockheed Martin F-35 Lightning II Incorporates Many Significant Technological Enhancements Derived from Predecessor Development Programs
AIAA AVIATION Forum 10.2514/6.2018-3368 June 25-29, 2018, Atlanta, Georgia 2018 Aviation Technology, Integration, and Operations Conference F-35 Air Vehicle Technology Overview Chris Wiegand,1 Bruce A. Bullick,2 Jeffrey A. Catt,3 Jeffrey W. Hamstra,4 Greg P. Walker,5 and Steve Wurth6 Lockheed Martin Aeronautics Company, Fort Worth, TX, 76109, United States of America The Lockheed Martin F-35 Lightning II incorporates many significant technological enhancements derived from predecessor development programs. The X-35 concept demonstrator program incorporated some that were deemed critical to establish the technical credibility and readiness to enter the System Development and Demonstration (SDD) program. Key among them were the elements of the F-35B short takeoff and vertical landing propulsion system using the revolutionary shaft-driven LiftFan® system. However, due to X- 35 schedule constraints and technical risks, the incorporation of some technologies was deferred to the SDD program. This paper provides insight into several of the key air vehicle and propulsion systems technologies selected for incorporation into the F-35. It describes the transition from several highly successful technology development projects to their incorporation into the production aircraft. I. Introduction HE F-35 Lightning II is a true 5th Generation trivariant, multiservice air system. It provides outstanding fighter T class aerodynamic performance, supersonic speed, all-aspect stealth with weapons, and highly integrated and networked avionics. The F-35 aircraft -
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. -
A Conceptual Design of a Short Takeoff and Landing Regional Jet Airliner
A Conceptual Design of a Short Takeoff and Landing Regional Jet Airliner Andrew S. Hahn 1 NASA Langley Research Center, Hampton, VA, 23681 Most jet airliner conceptual designs adhere to conventional takeoff and landing performance. Given this predominance, takeoff and landing performance has not been critical, since it has not been an active constraint in the design. Given that the demand for air travel is projected to increase dramatically, there is interest in operational concepts, such as Metroplex operations that seek to unload the major hub airports by using underutilized surrounding regional airports, as well as using underutilized runways at the major hub airports. Both of these operations require shorter takeoff and landing performance than is currently available for airliners of approximately 100-passenger capacity. This study examines the issues of modeling performance in this now critical flight regime as well as the impact of progressively reducing takeoff and landing field length requirements on the aircraft’s characteristics. Nomenclature CTOL = conventional takeoff and landing FAA = Federal Aviation Administration FAR = Federal Aviation Regulation RJ = regional jet STOL = short takeoff and landing UCD = three-dimensional Weissinger lifting line aerodynamics program I. Introduction EMAND for air travel over the next fifty to D seventy-five years has been projected to be as high as three times that of today. Given that the major airport hubs are already congested, and that the ability to increase capacity at these airports by building more full- size runways is limited, unconventional solutions are being considered to accommodate the projected increased demand. Two possible solutions being considered are: Metroplex operations, and using existing underutilized runways at the major hub airports. -
United States Rocket Research and Development During World War II
United States Rocket Research and Development During World War II Unidentified U.S. Navy LSM(R) (Landing Ship Medium (Rocket)) launching barrage rockets during a drill late in the Second World War. Image courtesy of the U.S. National Archives and Records Administration. and jet-assisted takeoff (JATO) units for piston-pow- Over the course of the Second World War, rockets ered attack fighters and bombers. Wartime American evolved from scientific and technical curiosities into rocket research evolved along a number of similar and practical weapons with specific battlefield applications. overlapping research trajectories. Both the U.S. Navy The Allied and Axis powers both pursued rocket re- and Army (which included the Army Air Forces) devel- search and development programs during the war. Brit- oped rockets for ground bombardment purposes. The ish and American rocket scientists and engineers (and services also fielded aerial rockets for use by attack their Japanese adversaries) mainly focused their efforts aircraft. The Navy worked on rocket-powered bombs on tactical applications using solid-propellant rockets, for antisubmarine warfare, while the Army developed while the Germans pursued a variety of strategic and the handheld bazooka antitank rocket system. Lastly, tactical development programs primarily centered on both the Army and Navy conducted research into JATO liquid-propellant rockets. German Army researchers units for use with bombers and seaplanes. Throughout led by Wernher von Braun spent much of the war de- the war, however, limited coordination between the veloping the A-4 (more popularly known as the V-2), armed services and federal wartime planning bodies a sophisticated long-range, liquid-fueled rocket that hampered American rocket development efforts and led was employed to bombard London and Rotterdam late to duplicated research and competition amongst pro- in the war. -
Aviation Acronyms
Aviation Acronyms 5010 AIRPORT MASTER RECORD (FAA FORM 5010-1) 7460-1 NOTICE OF PROPOSED CONSTRUCTION OR ALTERATION 7480-1 NOTICE OF LANDING AREA PROPOSAL 99'S NINETY-NINES (WOMEN PILOTS' ASSOCIATION) A/C AIRCRAFT A/DACG ARRIVAL/DEPARTURE AIRFIELD CONTROL GROUP A/FD AIRPORT/FACILITY DIRECTORY A/G AIR - TO - GROUND A/G AIR/GROUND AAA AUTOMATED AIRLIFT ANALYSIS AAAE AMERICAN ASSOCIATION OF AIRPORT EXECUTIVES AAC MIKE MONRONEY AERONAUTICAL CENTER AAI ARRIVAL AIRCRAFT INTERVAL AAIA AIRPORT AND AIRWAY IMPROVEMENT ACT AALPS AUTOMATED AIR LOAD PLANNING SYSTEM AANI AIR AMBULANCE NETWORK AAPA ASSOCIATION OF ASIA-PACIFIC AIRLINES AAR AIRPORT ACCEPTANCE RATE AAS ADVANCED AUTOMATION SYSTEM AASHTO AMERICAN ASSOCIATION OF STATE HIGHWAY & TRANSPORTATION OFFICIALS AC AIRCRAFT COMMANDER AC AIRFRAME CHANGE AC AIRCRAFT AC AIR CONTROLLER AC ADVISORY CIRCULAR AC ASPHALT CONCRETE ACAA AIR CARRIER ACCESS ACT ACAA AIR CARRIER ASSOCIATION OF AMERICA ACAIS AIR CARRIER ACTIVITY INFORMATION SYSTEM ACC AREA CONTROL CENTER ACC AIRPORT CONSULTANTS COUNCIL ACC AIRCRAFT COMMANDER ACC AIR CENTER COMMANDER ACCC AREA CONTROL COMPUTER COMPLEX ACDA APPROACH CONTROL DESCENT AREA ACDO AIR CARRIER DISTRICT OFFICE ACE AVIATION CAREER EDUCATION ACE CENTRAL REGION OF FAA ACF AREA CONTROL FACILITY ACFT AIRCRAFT ACI-NA AIRPORTS COUNCIL INTERNATIONAL - NORTH AMERICA ACID AIRCRAFT IDENTIFICATION ACIP AIRPORT CAPITAL IMPROVEMENT PLANNING ACLS AUTOMATIC CARRIER LANDING SYSTEM ACLT ACTUAL CALCULATED LANDING TIME Page 2 ACMI AIRCRAFT, CREW, MAINTENANCE AND INSURANCE (cargo) ACOE U.S. ARMY -
Advisory Circular 120-62
fw 3 Advisory U.S.Department of Transportation Federal Aviation Circular ’ AdminisWation Qlbject: TAKEOFF SAFETY TRAINING AID bte: g/Q/g4 AC No. 120-6.2 Announcement Of Availability Initiatedby: AFS-210 Change; 1 PURPOSE. This advisory circular (AC) announces the availability of a joint industry/Federal Aviation Administration (FAA) Takeoff Safety Training Aid to help air carriers and pilots increase safety during the takeoff phase of flight. a. The FAA recommends early consideration of the information contained in the aid and use of the material, as appropriate, for training aircrews. This AC also highlights certain key items, concepts, and definitions that each air carrier or operator should address in their respective operational procedures and crew qualification programs. b This circular applies to Federal Aviation Regulations (FAR) Part 121 operators. However, many of the principles, concepts, and procedures described apply to operations under FAR Parts 918 129, and 135 for certain aircraft, and are recommended for use by those operators when applicable. 2 BACKGROUND. Takeoff accidents resulting from improper rejected takeoff (RTO) decisions and procedures are significant contributors to worldwide commercial aviation accident statistics. For those takeoffs that are rejected, and for takeoffs made under certain environmental conditions and with certain system failures, risks could be reduced by a higher level of flightcrew knowledge and by the use of improved procedures. Due to the risks and the accident statistics associated with takeoffs, a joint FAA/industry team studied what actions might be taken to increase takeoff safety. These studies included simulation trials and in-depth analysis of takeoff accidents and incidents. -
A SEMI-EMPIRICAL METHODOLOGY for BALANCED FIELD LENGTH ESTIMATION of JET- ENGINED AIRCRAFT in EARLY DESIGN PHASES Tulio Angeiras Embraer S.A
A SEMI-EMPIRICAL METHODOLOGY FOR BALANCED FIELD LENGTH ESTIMATION OF JET- ENGINED AIRCRAFT IN EARLY DESIGN PHASES Tulio Angeiras Embraer S.A. and Aeronautical Technology Institute – ITA Product Development Engineer and Graduate Student Sao Jose dos Campos, SP, 12227-901, Brazil [email protected] Adson de Paula (ITA), Bento Mattos (ITA), Tarik Orra (Embraer) ABSTRACT Current levels of competitiveness displayed in business and commercial aviation market led to increasingly stringent performance and economy requirements. One of the key elements of these requirements is field performance, a factor that has great influence on the viability of certain route or operation for the aircraft in question, and that might shift the balance in a purchase decision. During early design phases, aerodynamic data about the aircraft being developed is often inaccurate and subject to changes during its evolution, which, alongside with difficulties do validate the results, renders numerical simulation methods unpractical for estimating field performance. These factors stimulated the development of a number of semi-empirical methodologies to estimate takeoff field lengths, of which some, by taking advantage of the available historical trend, produce very reasonable results and are widespread adopted on the aviation industry. Aiming to enable leaner aircraft designs, this paper presents an overview of several established methods, analyzing structure and comparing results obtained by their application to a databank of existing aircrafts. Finally, it -
Helioffshore Industry Safety Performance Report Here
Helicopter Safety Performance 2019 HeliOffshore Helicopter Safety Performance 2019 Section 1: Introduction and Background <2 2> Author: HeliOffshore Graphic Design: Avid Design Version: 1.0 Publication Date: December 2020 Disclaimer: While every effort has been made to ensure the information contained in this report is accurate, HeliOffshore makes no warranty, express or implied, and takes no responsibility as to the accuracy, capability, efficiency, merchantability, or functioning of this information. The user of such information does so at their own risk and has reviewed and independently verified the information for their own purposes. Extracts from this report, including values, graphs and figures, may be published without specific permission from HeliOffshore, provided that HeliOffshore is duly acknowledged as the source and that the material is reproduced accurately, in context and solely for the purpose of safety. HeliOffshore Helicopter Safety Performance 2019 Section 1: Introduction and Background 3 Introduction I am pleased to introduce the latest HeliOffshore Helicopter Safety Performance Report. In the following pages, you will find a unique, global, industry-wide perspective on the safety performance of the offshore aviation sector. Safety data is not always easy to read. It reveals our challenges and reminds us of our critical mission to transform global performance so no lives are lost in offshore aviation. This is a mission delivered by one evidence-based safety conversation at a time. Despite its breakthroughs and successes, it remains relentless work. Our industry frontline of pilots, engineers, maintainers, designers and passengers, deserve nothing less. So, thank you for your contribution to date. Thank you for sharing data and for your commitment to act on the priorities it reveals. -
Appendix a Description of Declared Distances
Appendix A Description of Declared Distances Declared distances at airports are a mechanism by which specific lengths of runway pavement are identified for use in aircraft operations. Declared distances are incorporated into the Operations Specifications of commercial aircraft operators that are part of the air carrier certificates and operations certificates issued by FAA under 14 CFR Part 119, as well as into the internal operations manuals of those operators. Pilots of commercial aircraft are required to comply with such specifications and manuals. The specified distance available for a particular operation such as landing may be different in each direction on the same runway pavement. The FAA defines four declared distances: • Takeoff Run Available (TORA) – the runway length declared available and suitable for satisfying takeoff run requirements. The TORA is measured from the start of takeoff to a point 200 feet from the beginning of the departure Runway Protection Zone. • Takeoff Distance Available (TODA) – this distance comprises the TORA plus the length of any remaining runway or clearway beyond the far end of the TORA. • Accelerate-Stop Distance Available (ASDA) – the runway plus stopway length declared available and suitable for the acceleration and deceleration of an aircraft that must abort its takeoff. A stopway is an area beyond the takeoff runway able to support the airplane during an aborted takeoff, without causing structural damage to the airplane. • Landing Distance Available (LDA) – the runway length that is declared available and suitable for satisfying aircraft landing distance requirements. The figure below illustrates how declared distances allow a runway pavement length of 11,600 feet to provide a usable runway length of 10,000 feet for landing and 10,600 feet for takeoffs in both directions while still providing the FAA-required runway safety area dimensions of 600 feet prior to the landing threshold and 1,000 feet beyond the runway end. -
(VL for Attrid
ECCAIRS Aviation 1.3.0.12 Data Definition Standard English Attribute Values ECCAIRS Aviation 1.3.0.12 VL for AttrID: 391 - Event Phases Powered Fixed-wing aircraft. (Powered Fixed-wing aircraft) 10000 This section covers flight phases specifically adopted for the operation of a powered fixed-wing aircraft. Standing. (Standing) 10100 The phase of flight prior to pushback or taxi, or after arrival, at the gate, ramp, or parking area, while the aircraft is stationary. Standing : Engine(s) Not Operating. (Standing : Engine(s) Not Operating) 10101 The phase of flight, while the aircraft is standing and during which no aircraft engine is running. Standing : Engine(s) Start-up. (Standing : Engine(s) Start-up) 10102 The phase of flight, while the aircraft is parked during which the first engine is started. Standing : Engine(s) Run-up. (Standing : Engine(s) Run-up) 990899 The phase of flight after start-up, during which power is applied to engines, for a pre-flight engine performance test. Standing : Engine(s) Operating. (Standing : Engine(s) Operating) 10103 The phase of flight following engine start-up, or after post-flight arrival at the destination. Standing : Engine(s) Shut Down. (Standing : Engine(s) Shut Down) 10104 Engine shutdown is from the start of the shutdown sequence until the engine(s) cease rotation. Standing : Other. (Standing : Other) 10198 An event involving any standing phase of flight other than one of the above. Taxi. (Taxi) 10200 The phase of flight in which movement of an aircraft on the surface of an aerodrome under its own power occurs, excluding take- off and landing.