<--- Back to Details
First PageDocument Content
Aerodynamics / Aeronautics / VTOL aircraft / VTOL / Wing configuration / Wingtip device / Lift-induced drag / V/STOL / Wing loading / Aviation / Aerospace engineering / Aircraft
Date: 2010-12-16 12:25:47
Aerodynamics
Aeronautics
VTOL aircraft
VTOL
Wing configuration
Wingtip device
Lift-induced drag
V/STOL
Wing loading
Aviation
Aerospace engineering
Aircraft

1 Design and aerodynamic considerations about the civil VTOL aircraft Ray

Add to Reading List

Source URL: www.rayaircraft.com

Download Document from Source Website

File Size: 948,84 KB

Share Document on Facebook

Similar Documents

  BACKGROUNDER No. 3140 | August 4, 2016  Operational Assessment of the F-35A Argues for Full Program

 BACKGROUNDER No. 3140 | August 4, 2016 Operational Assessment of the F-35A Argues for Full Program

DocID: 1ru36 - View Document

Aeronautics Educator Guide pdf

Aeronautics Educator Guide pdf

DocID: 1r49K - View Document

WHY ROTORS INSTEAD OF WINGS by Greg Gremminger When I first got into gyrocopters, I had been flying fixed-wing airplanes and ultralights for many years. What attracted me to gyros

WHY ROTORS INSTEAD OF WINGS by Greg Gremminger When I first got into gyrocopters, I had been flying fixed-wing airplanes and ultralights for many years. What attracted me to gyros

DocID: 1qGgr - View Document

GAO; F-35 JOINT STRIKE FIGHTER: Continued Oversight Needed as Program Plans to Begin Development of New Capabilities

GAO; F-35 JOINT STRIKE FIGHTER: Continued Oversight Needed as Program Plans to Begin Development of New Capabilities

DocID: 1qh67 - View Document

Aero Upgrade LLC Cost effective solutions for improving safety of flight and aircraft performance Services Provided: Avionics, engine, propeller and exhaust upgrades.  Aero Upgrade is a full service mainten

Aero Upgrade LLC Cost effective solutions for improving safety of flight and aircraft performance Services Provided: Avionics, engine, propeller and exhaust upgrades.  Aero Upgrade is a full service mainten

DocID: 1q57u - View Document