Effects of a Lower Surface Jet on the Lift-drag Ratio of a 45° Sweptback Wing at a Mach Number of 2.01 PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Effects of a Lower Surface Jet on the Lift-drag Ratio of a 45° Sweptback Wing at a Mach Number of 2.01 PDF full book. Access full book title Effects of a Lower Surface Jet on the Lift-drag Ratio of a 45° Sweptback Wing at a Mach Number of 2.01 by Emma Jean Landrum. Download full books in PDF and EPUB format.

Effects of a Lower Surface Jet on the Lift-drag Ratio of a 45° Sweptback Wing at a Mach Number of 2.01

Effects of a Lower Surface Jet on the Lift-drag Ratio of a 45° Sweptback Wing at a Mach Number of 2.01 PDF Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 44

Get Book Here

Book Description

Effects of a Lower Surface Jet on the Lift-drag Ratio of a 45° Sweptback Wing at a Mach Number of 2.01

Effects of a Lower Surface Jet on the Lift-drag Ratio of a 45° Sweptback Wing at a Mach Number of 2.01 PDF Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 44

Get Book Here

Book Description

Effects of a Lower Surface Jet on the Lift Drag Ratio of a 40 Degree Sweptback Wing at a Mach Number of 2.01

Effects of a Lower Surface Jet on the Lift Drag Ratio of a 40 Degree Sweptback Wing at a Mach Number of 2.01 PDF Author: Emma Jean Landrum
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

Get Book Here

Book Description

Transonic Flight Tests to Determine the Effect of Thickness Ratio and Plan-form Modification on the Zero-lift Drag of a 45© Sweptback Wing

Transonic Flight Tests to Determine the Effect of Thickness Ratio and Plan-form Modification on the Zero-lift Drag of a 45© Sweptback Wing PDF Author: William B. Pepper
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28

Get Book Here

Book Description

Effects of Wing Inboard Plan-form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-propelled Free-flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3

Effects of Wing Inboard Plan-form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-propelled Free-flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3 PDF Author: Allen B. Henning
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 32

Get Book Here

Book Description
An investigation was made to determine the effects of wing inboard plan-form modifications on the lift, drag, and longitudinal characteristics of a rocket-propelled free-flight model. The model had a body of fineness ration 17.4, a modified wing with a basic plan form swept back 52.5 degrees and an aspect ratio of 3, and inline horizontal tail surfaces which were aerodynamically pulsed continuously throughout the flight.

A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft

A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft PDF Author: James C. Williams
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 716

Get Book Here

Book Description
This report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.

Lift Induced on a Swept Wing by a Two-dimensional Partial-span Deflected Jet at Mach Numbers from 0.20 to 1.30

Lift Induced on a Swept Wing by a Two-dimensional Partial-span Deflected Jet at Mach Numbers from 0.20 to 1.30 PDF Author: Francis J. Capone
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76

Get Book Here

Book Description

NASA Contractor Report

NASA Contractor Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1366

Get Book Here

Book Description

A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0

A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 PDF Author: Robert S. Osborne
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20

Get Book Here

Book Description

Lift and Drag Characteristics at Subsonic Speeds and at a Mach Number of 1.9 of a Lifting Circular Cylinder with a Fineness Ratio of 10

Lift and Drag Characteristics at Subsonic Speeds and at a Mach Number of 1.9 of a Lifting Circular Cylinder with a Fineness Ratio of 10 PDF Author: Vernard E. Lockwood
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 26

Get Book Here

Book Description

Exploratory Investigation at Mach Numbers from 0.40 to 0.95 of the Effects of Jets Blown Over a Wing

Exploratory Investigation at Mach Numbers from 0.40 to 0.95 of the Effects of Jets Blown Over a Wing PDF Author: Lawrence Elwood Putnam
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76

Get Book Here

Book Description
An exploratory investigation has been made at Mach numbers from 0.40 to 0.95 to determine the effects on lift, drag, and pitching moment of blowing a jet exhaust over the upper surface of a 50 deg swept leading-edge wing. Also investigated were the effects of varying the longitudinal and vertical location of the nozzle exit on the induced effects of jet blowing.