Hallo! Tracked shipping to Netherlands with Delivery Duty Paid for just €7 

Ship to
Netherlands
0

My Account

  • argentina
  • chile
  • colombia
  • españa
  • méxico
  • perú
  • estados unidos
  • internacional

menu

Select your country

Americas

Europe

Rest of the world

portada Model for Vortex Ring State Influence on Rotorcraft Flight Dynamics
Type
Physical Book
Author
Publisher
Language
English
Pages
80
Format
Paperback
Dimensions
24.6 x 18.9 x 0.4 cm
Weight
0.16 kg.
ISBN13
9781287237013
Categories

Model for Vortex Ring State Influence on Rotorcraft Flight Dynamics

Wayne Johnson (Author) · Nasa Technical Reports Server (Ntrs) (Author) · Bibliogov · Paperback

Model for Vortex Ring State Influence on Rotorcraft Flight Dynamics - Nasa Technical Reports Server (Ntrs) ; Johnson, Wayne

New Book Imported to Netherlands
Delivery: 09 Sep - 16 Sep Shipping: 16 to 20 business days.
€ 28,84
Import costs and 9% BTW included in the price ✅
€ 28,84

Choose the list to add your product or create one New List

Go to My Wishlists
Calculate shipping cost

Synopsis "Model for Vortex Ring State Influence on Rotorcraft Flight Dynamics"

The influence of vortex ring state (VRS) on rotorcraft flight dynamics is investigated, specifically the vertical velocity drop of helicopters and the roll-off of tiltrotors encountering VRS. The available wind tunnel and flight test data for rotors in vortex ring state are reviewed. Test data for axial flow, non-axial flow, two rotors, unsteadiness, and vortex ring state boundaries are described and discussed. Based on the available measured data, a VRS model is developed. The VRS model is a parametric extension of momentum theory for calculation of the mean inflow of a rotor, hence suitable for simple calculations and real-time simulations. This inflow model is primarily defined in terms of the stability boundary of the aircraft motion. Calculations of helicopter response during VRS encounter were performed, and good correlation is shown with the vertical velocity drop measured in flight tests. Calculations of tiltrotor response during VRS encounter were performed, showing the roll-off behavior characteristic of tiltrotors. Hence it is possible, using a model of the mean inflow of an isolated rotor, to explain the basic behavior of both helicopters and tiltrotors in vortex ring state.

Customers reviews

More customer reviews
  • 0% (0)
  • 0% (0)
  • 0% (0)
  • 0% (0)
  • 0% (0)

Frequently Asked Questions about the Book

Is the book original?

All books in our catalog are Original.

In what language is the book written?

The book is written in English.

What is the format of this book?

The binding of this edition is Paperback.

Questions and Answers about the Book

Do you have a question about the book? Login to be able to add your own question.

Opinions about Bookdelivery

More customer reviews