LOW-LIFT DRAG AND STABILITY DATA FROM ROCKET MODELS OF A MODIFIED-DELTA-WING AIRPLANE WITH AND WITHOUT EXTERNAL STORES AT MACH NUMBERS FROM 0.8 TO 1.36 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 LOW-LIFT DRAG AND STABILITY DATA FROM ROCKET MODELS OF A MODIFIED-DELTA-WING AIRPLANE WITH AND WITHOUT EXTERNAL STORES AT MACH NUMBERS FROM 0.8 TO 1.36 PDF full book. Access full book title LOW-LIFT DRAG AND STABILITY DATA FROM ROCKET MODELS OF A MODIFIED-DELTA-WING AIRPLANE WITH AND WITHOUT EXTERNAL STORES AT MACH NUMBERS FROM 0.8 TO 1.36 by . Download full books in PDF and EPUB format.

LOW-LIFT DRAG AND STABILITY DATA FROM ROCKET MODELS OF A MODIFIED-DELTA-WING AIRPLANE WITH AND WITHOUT EXTERNAL STORES AT MACH NUMBERS FROM 0.8 TO 1.36

LOW-LIFT DRAG AND STABILITY DATA FROM ROCKET MODELS OF A MODIFIED-DELTA-WING AIRPLANE WITH AND WITHOUT EXTERNAL STORES AT MACH NUMBERS FROM 0.8 TO 1.36 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 54

Get Book Here

Book Description

LOW-LIFT DRAG AND STABILITY DATA FROM ROCKET MODELS OF A MODIFIED-DELTA-WING AIRPLANE WITH AND WITHOUT EXTERNAL STORES AT MACH NUMBERS FROM 0.8 TO 1.36

LOW-LIFT DRAG AND STABILITY DATA FROM ROCKET MODELS OF A MODIFIED-DELTA-WING AIRPLANE WITH AND WITHOUT EXTERNAL STORES AT MACH NUMBERS FROM 0.8 TO 1.36 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 54

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

Rocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Have a 60© Delta Wing and a High Unwept Horizontal Tail

Rocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Have a 60© Delta Wing and a High Unwept Horizontal Tail PDF Author: Robert F. Peck
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 32

Get Book Here

Book Description

Effect of External Stores on the Stability and Control Characteristics of a Delta Wing Fighter Model at Mach Numbers from 0.60 to 2.01

Effect of External Stores on the Stability and Control Characteristics of a Delta Wing Fighter Model at Mach Numbers from 0.60 to 2.01 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

Get Book Here

Book Description

Large-scale Flight Measurements of Zero-lift Drag and Low-lift Drag of 10 Wing-body Configurations at Mach Numbers from 0.8 to 1.6

Large-scale Flight Measurements of Zero-lift Drag and Low-lift Drag of 10 Wing-body Configurations at Mach Numbers from 0.8 to 1.6 PDF Author: John D. Morrow
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 58

Get Book Here

Book Description

Effect of Some Section Modifications and Protuberances on the Zero-lift Drag of Delta Wings at Transonic and Supersonic Speeds

Effect of Some Section Modifications and Protuberances on the Zero-lift Drag of Delta Wings at Transonic and Supersonic Speeds PDF Author: Carl A. Sandahl
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48

Get Book Here

Book Description

Comparison of Low-lift Drag at Mach Numbers from 0.74 to 1.37 of Rocket-boosted Models Having Externally Braced Wings and Cantilever Wings

Comparison of Low-lift Drag at Mach Numbers from 0.74 to 1.37 of Rocket-boosted Models Having Externally Braced Wings and Cantilever Wings PDF Author: Waldo L. Dickens
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 22

Get Book Here

Book Description
An investigation has been conducted to determine whether the low-lift drag of a rocket-model airplane-like configuration could be reduced at transonic and low supersonic Mach numbers by reducing the wing thickness while external braces were used to provide the necessary bending strength. The investigation consisted of flight training two rocket models having aspect ratio 3.04, unswept braced tapered wings mounted on fuselages with the same fineness ratios and cross-sectional area distributions. Data collected from the flight test of a model having a thicker cantilever wing of the same plan form were compared with data collected in this investigation.

Flight Determination of the Drag and Longitudinal Stability and Control Characteristics of a Rocket-powered Model of a 60 Degrees Delta-wing Airplane from Mach Numbers of 0.75 to 1.70

Flight Determination of the Drag and Longitudinal Stability and Control Characteristics of a Rocket-powered Model of a 60 Degrees Delta-wing Airplane from Mach Numbers of 0.75 to 1.70 PDF Author: Grady L. Mitcham
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

Get Book Here

Book Description

Free-flight Investigation to Obtain Drag-at-lift and Stability Data for a 60 Degree Delta-wing-body Configuration Over a Mach Number Range of 1.3 to 1.6

Free-flight Investigation to Obtain Drag-at-lift and Stability Data for a 60 Degree Delta-wing-body Configuration Over a Mach Number Range of 1.3 to 1.6 PDF Author: Clement J. Welsh
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 23

Get Book Here

Book Description
Flight tests have been made of a rocket-propelled 60 degree delta-wing-body configuration; the wing airfoil section was NACA 0003-63. Drag at lift and stability data were obtained for a Mach number range of 1.28 to 1.6.

Introduction to Aircraft Flight Mechanics

Introduction to Aircraft Flight Mechanics PDF Author: Thomas R. Yechout
Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666

Get Book Here

Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.