<--- Back to Details
First PageDocument Content
Thrust-to-weight ratio / European Aviation Safety Agency / Europe / Transport / Aviation / Pusher configuration
Date: 2015-05-15 18:44:39
Thrust-to-weight ratio
European Aviation Safety Agency
Europe
Transport
Aviation
Pusher configuration

EASA ED DecisionR CS-25 Amendment 1

Add to Reading List

Source URL: www.easa.europa.eu

Download Document from Source Website

File Size: 3,10 MB

Share Document on Facebook

Similar Documents

Technology / Energy / Aerodynamics / Turbofan / Turboprop / Wing loading / Thrust-to-weight ratio / Bypass ratio / Specific thrust / Jet engines / Gas turbines / Fluid dynamics

27TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES COMPARISON OF POWERED-LIFT TURBOFAN AIRCRAFT WITH CONVENTIONAL TURBOPROP AIRCRAFT FOR ESTOL APPLICATION Corin Gologan, Dieter Schmitt

DocID: 19iFN - View Document

Aviation / Stall / Propeller / Aircraft / Thrust-to-weight ratio / Ducted fan / Thrust / Flight / Aerospace engineering / Aerodynamics / Fluid dynamics

JOURNAL OF AIRCRAFT Vol. 47, No. 3, May–June 2010 Engineering Notes Optimization of Hover-to-Cruise Transition Maneuver Using

DocID: 187EW - View Document

Thrust-to-weight ratio / European Aviation Safety Agency / Europe / Transport / Aviation / Pusher configuration

EASA ED DecisionR CS-25 Amendment 1

DocID: 16Vlv - View Document

Fighter aircraft / Aerospace engineering / Aircraft / Aviation / McDonnell Douglas F-15 Eagle / Wing loading / Thrust-to-weight ratio

F-15C fires an AIM-120 AAMRAM Missile RIAC Success Story F-15 Wing Metallographic Analysis www.theRIAC.org

DocID: JssM - View Document

302d Fighter Squadron / Lockheed Martin F-22 Raptor / Joint Base Elmendorf-Richardson / Air Force Reserve Command / Oliver Goodall / Freeman Field Mutiny / United States / 477th Fighter Group / Tuskegee Airmen

Stealthy supercruise, maneuverability integrated avionicsfirstkill low-observable sleekaerodynamicdesign, increased thrust stealthYadvanced flightcontrols thrust vectoring high thrust-to-weight ratio AIR DOMINANCE

DocID: kDrm - View Document