Wind-tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1/62-scale Model of the X-1E at Supersonic Speeds

Wind-tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1/62-scale Model of the X-1E at Supersonic Speeds PDF Author: Arthur Henderson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 94

Get Book Here

Book Description
An investigation to determine the static longitudinal and lateral stability characteristics of a 1/62-scale model of the X-1E has been conducted in the Langley 9-inch supersonic tunnel. Tests were made at Mach numbers of 1.62, 1.94, 2.22, 2.40, and 2.62 on the wing-body, wing-body-vertical-tail, and complete model configurations. Detailed analysis of the test results has not been made.

Wind-tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1/62-scale Model of the X-1E at Supersonic Speeds

Wind-tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1/62-scale Model of the X-1E at Supersonic Speeds PDF Author: Arthur Henderson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 94

Get Book Here

Book Description
An investigation to determine the static longitudinal and lateral stability characteristics of a 1/62-scale model of the X-1E has been conducted in the Langley 9-inch supersonic tunnel. Tests were made at Mach numbers of 1.62, 1.94, 2.22, 2.40, and 2.62 on the wing-body, wing-body-vertical-tail, and complete model configurations. Detailed analysis of the test results has not been made.

Wind-tunnel Investigation of Static Lateral and Longitudinal Stability Characteristics of a 1/62-scale Model of the X-1E Airplane at Combined Angles of Attack and Sideslip at Supersonic Speeds

Wind-tunnel Investigation of Static Lateral and Longitudinal Stability Characteristics of a 1/62-scale Model of the X-1E Airplane at Combined Angles of Attack and Sideslip at Supersonic Speeds PDF Author: Arthur Henderson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 26

Get Book Here

Book Description
An investigation to determine the static longitudinal and lateral stability characteristics of a 1/62-scale model of the X-1E airplane combined angles of attack and sideslip has been conducted in the Langley 9-inch supersonic tunnel. Tests were made at Mach numbers of 1.62, 1.94, 2.22, 2.40, and 2.62 on the complete model configuration. Detailed analysis of the test results has not been made in order to expedite publication of the data.

Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448

Get Book Here

Book Description


A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296

Get Book Here

Book Description


Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 494

Get Book Here

Book Description


Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :

Get Book Here

Book Description


Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860

Get Book Here

Book Description


NASA Memorandum

NASA Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 66

Get Book Here

Book Description


Wind-tunnel Investigation of the Static Stability of a 1/56-scale Model of the X-1E Airplane at Mach Numbers of 2.37, 2.98, and 4.01

Wind-tunnel Investigation of the Static Stability of a 1/56-scale Model of the X-1E Airplane at Mach Numbers of 2.37, 2.98, and 4.01 PDF Author: Fred M. Smith
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 124

Get Book Here

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1222

Get Book Here

Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.