F-16 aircraft
Flow Analysis over an F-16 Aircraft Using Computational Fluid Dynamics
... moving aircraft with a high lift coefficient and low drag coefficient, which helps them to enhance their military force and strengthens its civilization’s ...the F-16 aircraft using computer ...
5
Linear Parameter-Varying Control of an F-16 Aircraft at High Angle of Attack
... Most aircraft spend most of their flying time in a wings-level steady-state flight ...tudinal F-16 aircraft model based on NASA Langley Research Center (LaRC) wind tunnel tests ...the ...
145
Study the effect of ice accretion on various aerodynamic flight characteristics using F 16 model
... any aircraft safety. A major rolling parameter in the criteria of aircraft icing is the ice roughness which indicates surface roughness induced with the initial stages of in- flight ice ...
9
Verification Challenges in F-16 Ground Collision Avoidance and Other Automated Maneuvers
... We have presented three benchmark scenarios of increasing complexity dealing with various aspects of control of an F-16 aircraft. For each benchmark, several sets of initial states were provided, and ...
10
System Modeling and Controller Design for Lateral and Longitudinal Motion of F-16
... Abstract: Classical control laws are still widely used in aviation industry because of their good structural understanding, simplicity, and better tracking control performance. However in recent decades the application ...
7
Simulation of the Tanjung Kupang Air Crash
... the aircraft, indicating that the pilot or the co-pilot was in full awareness of the situation and still trying hard as possible to handle the critical ...the aircraft or possibly were ...
8
Framework for predicting noise power distance curves for novel aircraft designs
... future aircraft concepts, such as the Turboelec- tric DP (TeDP)[39] and Universally-Electric [40] aircraft that consist of a power unit (turboshaft and batteries respectively) that drives electrically, ...
34
CFD and VLM Simulation of the Novel Twin body Asymmetric Flying wing Aircraft
... twin-body aircraft has the advantages of heavy load and long range, maneuverability is its ...twin-body aircraft is in a complex airflow environment, the stable flight state is likely to be ...of ...
7
A 10 BIT 50 MS/S LOW POWER PIPELINE ADC FOR WIMAX/LTE
... the aircraft stays steady, which proves the structure of two propellers can offset the reverse torque ...the aircraft is not homogeneous because of machining inaccuracy and assembling errors, that’s the ...
7
The European aerospace industry. Trading position and figures 1994. III/4001/94-EN, 1 April 1994
... The European Aerospace Industry Trading Position and Figures - 1994 CIVIL TRANSPORT AIRCRAFT The figures relating to the civil jet aircraft orders, deliveries and backlogs [aircraft orde[r] ...
256
Airborne observations of formic acid using a chemical ionization mass spectrometer
... (NI-CIMS) has proven to be a powerful method for sensi- tive and selective measurements of organic acids at the ppt level (Amelynck et al., 2000; Crounse et al., 2006; Paulot et al., 2009a, b). More recently, Veres et ...
11
Design and CFD Analysis of Air Foil
... such as air or water. It is used in the drag equation where a lower drag coefficient indicates the object will have less aerodynamic or drag. The drag coefficients always associated with a particular surface area. The ...
5
Synergistic Behavior of Mixed Monolayer/Mixed Micelle Formation between Cationic Monomeric and Dimeric Surfactants with PEO-PPO-PEO Triblock Copolymer
... (Pluronic F-127) with cationic monomeric (hexadecyltrimethylammonium bromide), and gemini or dimeric (Pentanediyl-1, 5-bis (dimethylcetylammonium bromide)) surfactants was investigated using surface tension and ...
12
The European aerospace industry 1998 statistical survey
... Breakdown of 1998 EU Aerospace Industry Turnover~~ by Product Segment Total: 62,2 Billion ECU Space+ 7,9% Aircraft Maintenance 22,5% Aircraft Final Products+!> 4 I ,5% Military Aircraft [r] ...
14
Mean flow and turbulence measurements in the near field of a fighter aircraft wing-tip vortex at high Reynolds number and transonic flow conditions
... There has been renewed interest in studying the formation, structure and development of aircraft wing-tip vortices. These trailing vortices can be a serious hazard for smaller, following aircraft. Although ...
10
Quantitative risk assessment on fire and explosion impacts for nuclear power plants
... o f VCE involving aircraft crash on the nuclear ...o f the explosion characteristics and its impact on o f Structures, Systems, and Components (SSCs) is important in determining the ...
48
The European aerospace industry - trading position and figures. III/537/88-EN (final), 1 February 1988
... For each category of aircraft, the following tables are given: - absolute value, - geographical breakdown of total aircraft -market share of EEC 12-built aircraft Cas~ Cas~ of world tota[r] ...
245
The European aerospace industry: Trading position and figures 1997
... Cll'IL TRANSPORT AIRCRAFT TABLE2.15 CIVIL TRANSPORT AIRCRAFT ANNUAL DELIVERIES Category: Short/Medium-haul Turboprop Distribution of aircraft by geographical area EU-buiH share of deiver[r] ...
240
Emerging Energy Storage Solutions for Transportation Electrification – A Review
... Grojo, “Influence of the energy management on the sizing of electrical energy storage systems in an aircraft,” Journal of Power Sources, vol. Verde, “Sizing of a solar/hydrogen system f[r] ...
16
Design and Simulation of a Moving-magnet-type Linear Synchronous Motor for Electromagnetic Launch System
... Electromagnetic Aircraft Launch System (EMALS) is the US Navy’s next generation aircraft launching system for the twenty first century aircraft ...handle aircraft at a much wider range of ...
6