Analysis of the Aerodynamic Coefficients for the Evolvable Demonstrator for Upset Recovery Approaches with Evaluation in the Wind-tunnel - Archive ouverte HAL Accéder directement au contenu
Pré-Publication, Document De Travail Année :

Analysis of the Aerodynamic Coefficients for the Evolvable Demonstrator for Upset Recovery Approaches with Evaluation in the Wind-tunnel

(1) , (1) , (1)
1
Torbjørn Cunis
  • Fonction : Auteur
  • PersonId : 1035111
Murat Bronz

Résumé

While in-flight loss of control has remained a severe threat to aviation, few of the upset recovery approaches designed by aeronautical research has been demonstrated in flight tests. Enabled by the ongoing success of micro air vehicles, we discuss the concept of an aerial experimental platform for upset recovery, EDURA (Evolvable Demonstrator for Upset Recovery Approaches), allowing cheap and flexible flight demonstrations. The aerodynamic coefficients of the vehicle presented here are numerically computed and extended to a full-envelope aerodynamic model using piece-wise polynomials in pre-and post-stall. Eventually, the aerodynamics are verified with wind-tunnel force measurements for a 3D-printed mock-up.
Fichier principal
Vignette du fichier
paper-edura.pdf (4.75 Mo) Télécharger le fichier
Origine : Fichiers produits par l'(les) auteur(s)
Loading...

Dates et versions

hal-01857275 , version 1 (14-08-2018)

Identifiants

  • HAL Id : hal-01857275 , version 1

Citer

Torbjørn Cunis, Murat Bronz, Jean-Philippe Condomines. Analysis of the Aerodynamic Coefficients for the Evolvable Demonstrator for Upset Recovery Approaches with Evaluation in the Wind-tunnel. 2018. ⟨hal-01857275⟩
84 Consultations
521 Téléchargements

Partager

Gmail Facebook Twitter LinkedIn More