The Aerodynamics of Delta Wings of Elliptical Cross-section with Separated Flow

The Aerodynamics of Delta Wings of Elliptical Cross-section with Separated Flow
Author :
Publisher :
Total Pages : 80
Release :
ISBN-10 : STANFORD:36105046324096
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis The Aerodynamics of Delta Wings of Elliptical Cross-section with Separated Flow by : Joint Institute for Aeronautics and Acoustics. Joint Institute for Aeronautics and Acoustics

Download or read book The Aerodynamics of Delta Wings of Elliptical Cross-section with Separated Flow written by Joint Institute for Aeronautics and Acoustics. Joint Institute for Aeronautics and Acoustics and published by . This book was released on 1985 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:


The Aerodynamics of Delta Wings of Elliptical Cross-section with Separated Flow Related Books

The Aerodynamics of Delta Wings of Elliptical Cross-section with Separated Flow
Language: en
Pages: 80
Authors: Joint Institute for Aeronautics and Acoustics. Joint Institute for Aeronautics and Acoustics
Categories:
Type: BOOK - Published: 1985 - Publisher:

DOWNLOAD EBOOK

Separated and Vortical Flow in Aircraft Wing Aerodynamics
Language: en
Pages: 458
Authors: Ernst Heinrich Hirschel
Categories: Technology & Engineering
Type: BOOK - Published: 2020-10-04 - Publisher: Springer Nature

DOWNLOAD EBOOK

Fluid mechanical aspects of separated and vortical flow in aircraft wing aerodynamics are treated. The focus is on two wing classes: (1) large aspect-ratio wing
Vortex Flows at Supersonic Speeds
Language: en
Pages: 104
Authors: Richard M. Wood
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 2003 - Publisher:

DOWNLOAD EBOOK

A Theoretical Investigation of the Aerodynamics of Slender Wing-body Combinations Exhibiting Leading-edge Separation
Language: en
Pages: 124
Authors: Alvin H. Sacks
Categories: Aerodynamic load
Type: BOOK - Published: 1967 - Publisher:

DOWNLOAD EBOOK

A theoretical analysis is presented for calculating the normal force and center of pressure on plane wing/body combinations exhibiting leading edge separation.
Reduction of Drag Due to Lift at Supersonic Speeds
Language: en
Pages: 124
Authors: Douglas Aircraft Company
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1955 - Publisher:

DOWNLOAD EBOOK

$EVERAL TOPICS RELATING TO THE REDUCTION OF DRAG DUE TO LIFT AT SUPERSONIC SPEEDS ARE DISCUSSED. The distribution of camber for optimial loading of diamond plan