spacephotos.com Home page
DISCOUNT :     Ref T39 : Télescope PERL 114/1000                Ref T41 : Télescope PERL 114/900                Ref PP070 : Saturnian System - Voyager                Ref ALEM01 : The set of 18 Middle size model Aviation Badges                Ref DC1 : SPOT : EARTH OBSERVATION SATELLITE - 12 slides set                Ref LCN01 : The set of 2 caps                Ref SF1014 : A retractable Chrome Plated Fisher Space Pen                
 Our Picture Library
 Retailers space
 Our products
 Photo Prints
Fisher Space Pen
 Observation Instruments
   Telescopes
   Refractor Telescopes
   Binoculars
   Planetariums
 Posters
NASA Caps
 Slides
 Message to E.T.
 Wall Charts
 Post Cards
 Aviation Badges

 Products listing
 Our favourite links
Association Drômoise d'Astronomie Les Pleiades


*****************

 Quick Find
 
Advanced Search
 Newsletter



 
Unsubscribe
 Information
Shipping & Returns
Privacy Notice
Contact Us

PageRank
PageRank Actuel
 
Home »  Photo Prints » Aviation-NASA aircrafts-Prototypes » S04670
 
Ref S04670 : Structural loads testing on the Active Aeroelastic Wing F-18 in the Flight Loads Laboratory at NASA's Dryden flight Research Center, Edwards, California
    



Select in the form below the print format
you would like to order

DIMENSIONS High Definition PRINT BACKLIT*
40 x 60 cm
15.7 x 23.6 inches
23.00 € 20.70 €
125.00 €
50 x 75 cm
19.7 x 29.5 inches
29.90 € 26.91 €
140.00 €
60 x 90 cm
23.6 x 35.4 inches
45.00 € 40.50 €
170.00 €
80 x 120 cm
31.5 x 47.2 inches
75.00 €
220.00 €
100 x 150 cm
39.4 x 59.1 inches
109.00 €
290.00 €

*Backlit is a translucent matter to apply in front of a neon light
Thème : Aviation-NASA aircrafts-Prototypes

Description :

Structural loads testing on the Active Aeroelastic Wing F-18 has begun in the Flight Loads Laboratory at NASA's Dryden flight Research Center, Edwards, California. The heavily modified and instrumented F-18A entered the Loads Lab in mid-March, 2001, for fit checks of loads hardware and instrumentation checkout prior to initiation of actual structural loads testing. The F-18A will be undergoing loads testing on its modified wings for almost six months, followed by extensive systems tests and simulation before flight tests begin. The AAW project goal is to demonstrate improved aircraft roll control through aerodynamically-induced wing twist on a full-scale aircraft. The F-18A has been modified with additional actuators, a split leading edge flap and thinner wing skins. The traditional wing control surfaces—trailing edge ailerons and the outboard leading edge flaps—are used to provide the aerodynamic force needed to twist or ''warp'' the wing. AAW research could enable thinner, higher aspect-ratio wings on future aircraft which could result in reduced aerodynamic drag, allowing greater range or payload and improved fuel efficiency.


 Customers who bought this product also purchased

Ref S01349 : River seen from space

Ref S02584 : Galactic Silhouettes

Ref T01263 : Greece October 1989

Ref T91GPE : PERL VIXEN TELESCOPE 114/900 GPE

Ref E062 : Aviation Badge

Ref L99.1 : HIGH LANDER Prominar visée à 45°

Ref T123GP-DM : Lunette FL 106/920

Ref LSF01 : The set of the 7 Fisher Space Pens at a promotional price. Each pen is delivered in a gift case
 My account
 Create an account
 My Shopping Cart
Your Shopping Cart is Empty
 Languages        
 Tell A Friend
 
 Specials

Ref T27 : Sky-Watcher 130/900

360.00 € - 314.00 €
 What's New?

Ref T39 : Télescope PERL 114/1000

285.00 € - 278.00 €290.0000
 Currencies
 Reviews
 Write a review on this product!
 Bestsellers

Ref T27 : Sky-Watcher 130/900
360.00 € - 314.00 €