<--- Back to Details
First PageDocument Content
Aerodynamics / Disk loading / Rotorcraft / Tiltrotor / Helicopter / Wingtip device / Wing loading / Lift-to-drag ratio / Lift-induced drag / Aerospace engineering / Aircraft / Aviation
Date: 2014-06-09 16:38:04
Aerodynamics
Disk loading
Rotorcraft
Tiltrotor
Helicopter
Wingtip device
Wing loading
Lift-to-drag ratio
Lift-induced drag
Aerospace engineering
Aircraft
Aviation

Aerodynamic Limits on Large Civil Tiltrotor Sizing and Efficiency

Add to Reading List

Source URL: rotorcraft.arc.nasa.gov

Download Document from Source Website

File Size: 2,13 MB

Share Document on Facebook

Similar Documents

09 JanuaryZK-GDG Tail Weight Loading Chart with No wing water ballast, No tail water ballast, No baggage and No front seat weight ballasting only – for other configurations a modified chart is required.

DocID: 1rznf - View Document

Aeronautics / Air sports / Aviation / Adventure travel / Individual sports / Paragliding / Aerodynamics / Glider / Wing loading / Gliding / Powered hang glider / Hang gliding

Page 1 Page 2 Verification of Checks and repairs

DocID: 1qJcG - View Document

Biology / Aviculture / Measurement / Bird behavior / Bird flight / Bird / Analysis of covariance / Aviary / Ornithology / Wing loading / Great tit / Allometry

ANIMAL BEHAVIOUR, 2006, 72, 663e672 doi:j.anbehavEffects of wing area reduction on winter body mass and foraging behaviour in coal tits: field and aviary experiments LUI S M. C ARR AS CA L & VIC ENT

DocID: 1pWK0 - View Document

Aerodynamics / Gliding / Variometer / Glider / Lift / Gliding flight / Wing loading / Stall / Banked turn / Slip / Rate of climb / Thermal

Microsoft Word - Intro. to X-C.pub 2006.doc

DocID: 1pDPy - View Document

Aerodynamics / Gliding / Variometer / Glider / Lift / Gliding flight / Wing loading / Stall / Banked turn / Slip / Rate of climb / Thermal

Microsoft Word - Intro. to X-C.pub 2006.doc

DocID: 1pptt - View Document