Relevant bibliographies by topics / Harrier II/AV-8B/GR5

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Academic literature on the topic 'Harrier II/AV-8B/GR5'

Author: Grafiati
Published: 4 June 2021
Last updated: 28 July 2025

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Journal articles on the topic "Harrier II/AV-8B/GR5"

1

Riley, B. L. "AV-SB/GR Mk 5 Airframe Composite Applications." Proceedings of the Institution of Mechanical Engineers, Part D: Transport Engineering 200, no. 3 (1986): 167–83. http://dx.doi.org/10.1243/pime_proc_1986_200_178_02.

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This paper describes the composite applications on the AV-8B/GR Mk 5 Harrier II airfame. Twenty-five per cent of the airframe weight is composite materials resulting in a weight saving of 525 lb per aircraft. Topics covered in this paper include the composite wing, forward fuselage and horizontal tail designs, the development test programmes, design philosophy, interpretation and evaluation of test results, impact damage, ballistic damage, lightning, repairs, and manufacturing defects.
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Groll, D. B., and T. R. Bossart. "Practical Design Considerations for Integrating the Propulsion System With the Aircraft for Jetborne Flight." Journal of Engineering for Gas Turbines and Power 112, no. 2 (1990): 192–98. http://dx.doi.org/10.1115/1.2906161.

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Results of a pilot-in-the-loop simulator evaluation for engine and configuration variations to the AV-8B Harrier II aircraft are presented. Configurations were tested for various center of gravity locations, weights, pitching moments of inertia, and thrust center locations in jetborne flight. The effects of the propulsion system’s characteristics in relation to aircraft parameters are generalized with regard to pitch handling qualities such as control power, pitch sensitivity, disturbance susceptibility, and control margin. A proposed modification to improve pitch handling qualities also was e
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3

Jiniraj, R., T. Logesh, and D. Rajapatel. "Leading Edge Shape Optimization of Whitcomb IL Airfoil in Transonic Flow Using a Multi-Objective Genetic Algorithm (MOGA)." International Journal of Vehicle Structures and Systems 13, no. 1 (2021). http://dx.doi.org/10.4273/ijvss.13.1.18.

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Leading edge shape optimization of transonic airfoils requires creating an airfoil surface that reduces the drag divergence due to transonic shocks by either delaying them or reducing their strength at a given transonic cruise speed while maintaining the lift. Aircrafts like Boeing 757, Airbus A300, Boeing 777 and McDonnell Douglas AV-8B Harrier II use Whitcomb IL supercritical airfoil for efficient aerodynamic performance in transonic conditions. This study employs a multi-objective genetic algorithm for shape optimization of leading edge of the Whitcomb IL airfoil to achieve three objectives
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Books on the topic "Harrier II/AV-8B/GR5"

1

BAE Harrier GR7/GR9 and Boeing AV-8B Harrier II Plus: Aircraft in Detail. HMH Publications, 2020.

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2

Chesneau, Roger. Aeroguide 16: McDonnell Douglas AV-8B Harrier II. Linewrights Ltd., 1987.

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3

Nordeen, Lon. AV-8b Harrier II Units of Operation Enduring Freedom. Bloomsbury Publishing Plc, 2014.

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AV-8B Harrier II Units of Operation Enduring Freedom. Bloomsbury Publishing Plc, 2012.

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Laurier, Jim, and Lon Nordeen. AV-8B Harrier II Units of Operation Enduring Freedom. Bloomsbury Publishing Plc, 2014.

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Laurier, Jim, and Lon Nordeen. AV-8B Harrier II Units of Operation Enduring Freedom. Bloomsbury Publishing Plc, 2014.

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Laurier, Jim, and Lon Nordeen. AV-8B Harrier II Units of Operation Iraqi Freedom I-VI. Bloomsbury Publishing Plc, 2012.

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AV-8B Harrier II Units of Operation Iraqi Freedom I-VI. Bloomsbury Publishing Plc, 2013.

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9

Neubeck, Ken. AV-8B Harrier II: The US Marine Corps' VSTOL Jet Aircraft. Schiffer Publishing, Limited, 2022.

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AV-8B Harrier II Units of Operation Iraqi Freedom I-VI. Bloomsbury Publishing Plc, 2013.

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Conference papers on the topic "Harrier II/AV-8B/GR5"

1

Hirschberg, Michael. "A Humble Public Servant: Hal Andrews (1924–2007)." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-54.

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Harold (Hal) Andrews, a US Navy veteran and Naval Aviation technical leader, joined what is now known as the Naval Air Systems Command (NAVAIR) in 1955. There, Andrews held responsibilities for nearly 50 types of US Navy, Marine or joint aircraft prior to his retirement in 1986 as NAVAIR's Technical Director of Research and Technology. Andrews was an expert in Naval Aviation history, and a stickler for accuracy. By 1960, he was a contributing editor and technical advisor to the Navy's magazine, Naval Aviation News, in his spare time. He was also an advisor to several naval aviation association
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2

Cunningham, William H., and Joseph F. Boytos. "Navy V/STOL Engine Experience in Altitude Test Facility." In ASME 1988 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1988. http://dx.doi.org/10.1115/88-gt-317.

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The Pegasus V/STOL Engine used in the AV-8B/GR MK5 Harrier II Aircraft presents several unique installation requirements for testing in an Altitude Test Facility. These requirements are dictated by the fact that the Pegasus engine has four separate exhaust nozzles, and the short, highly-curved Harrier inlet creates unusual inlet distortion conditions. The Naval Air Propulsion Center has designed and fabricated equipment which has been used to test the Pegasus engine under simulated altitude conditions. During engine testing, problems were encountered with the rear nozzle exhaust collectors and
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3

MUFFLER, R. "AV-8B Harrier II training capabilities." In Flight Simulation Technologies Conference. American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-1734.

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4

Mathews, Roger H. "Near Term Enhancements of the AV-8B Harrier II." In SAE International Powered Lift Conference and Exposition. SAE International, 1987. http://dx.doi.org/10.4271/872321.

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5

Migbee, V. L., G. G. Gaston, and K. W. Gibbar. "A Highly Monitored AV-8B Harrier II Digital Flight Control System." In SAE International Powered Lift Conference and Exposition. SAE International, 1987. http://dx.doi.org/10.4271/872332.

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6

TINGER, HERBERT. "Analysis and application of aircraft departure prediction criteria to the AV-8B Harrier II." In 14th Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-2561.

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7

MYSKO, STEPHEN, WEI CHYU, MICHAEL STORTZ, and CHUEN-YEN CHOW. "Navier-Stokes simulation of external/internal transonic flow on the forebody/inlet of the AV-8B Harrier II." In 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-3057.

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8

Groll, D. B., and T. R. Bossart. "Practical Design Considerations for Integrating the Propulsion System With the Aircraft for Jetborne Flight." In ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1989. http://dx.doi.org/10.1115/89-gt-310.

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Abstract:
Results of a pilot-in-the-loop simulator evaluation for engine and configuration variations to the AV-8B Harrier II aircraft are presented. Configurations were tested for various center of gravity locations, weights, pitching moments of inertia, and thrust center locations in jetborne flight. The effects of the propulsion system’s characteristics in relation to aircraft parameters are generalized with regard to pitch handling qualities such as control power, pitch sensitivity, disturbance susceptibility, and control margin. A proposed modification to improve pitch handling qualities was also e
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