Effect of Body-Mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Deg Swept Wing at Mach Numbers from 0.80 to 0.98

Effect of Body-Mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Deg Swept Wing at Mach Numbers from 0.80 to 0.98 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 80

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Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Degree Swept Wing at Mach Numbers from 0.80 to 0.98

Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Degree Swept Wing at Mach Numbers from 0.80 to 0.98 PDF Author: F. E. West
Publisher:
ISBN:
Category :
Languages : en
Pages : 76

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Force Tests Results for Body-mounted Lateral Controls and Speed Brakes on a 45 Degree Swept-wing Model at Mach Numbers from 0.80 to 0.98

Force Tests Results for Body-mounted Lateral Controls and Speed Brakes on a 45 Degree Swept-wing Model at Mach Numbers from 0.80 to 0.98 PDF Author: F. E. West
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32

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An investigation has been made in the Langley 16-foot transonic tunnel to determine the aerodynamic characteristics of several body-mounted lateral-control and speed-brake configurations. The basic model had a 45 degree swept wing with an aspect ratio of 3. Six-component balance data were obtained at Mach numbers of 0.80, 0.94, and 0.98 for angles of attack that usually ranged from about zero to 21 degrees.

The Journal of the Royal Aeronautical Society

The Journal of the Royal Aeronautical Society PDF Author: Royal Aeronautical Society
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 972

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Beyond Tube-and-Wing

Beyond Tube-and-Wing PDF Author: Bruce Larrimer
Publisher:
ISBN: 9781626830592
Category :
Languages : en
Pages :

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Effects of Body Camber on Aerodynamic Characteristics of a Lifting Entry Vehicle Model at Mach Numbers from 2.30 to 4.62

Effects of Body Camber on Aerodynamic Characteristics of a Lifting Entry Vehicle Model at Mach Numbers from 2.30 to 4.62 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52

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From Archangel to Senior Crown

From Archangel to Senior Crown PDF Author: Peter W. Merlin
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : History
Languages : en
Pages : 240

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Book Description
The Lockheed Blackbirds hold a unique place in the development of aeronautics. In their day, the A-12, YF-12, M-21, D-21, and SR-71 variants outperformed all other jet airplanes in terms of altitude and speed. Now retired, they remain the only production aircraft capable of sustained Mach 3 cruise and operational altitudes above 80,000 feet.This is the first book to address the technical aspects of these incredible aircraft. The author describes the design evolution of the Blackbird, from the Archangel to the Senior Crown (the Air Force's SR-71.) He describes in detail the construction and materials challenges faced by Lockheed, as well as the Blackbird's performance characteristics and capabilities.A NASA historian, the author describes NASA's role in using the aircraft as a flying laboratory to collect data on materials, structures, loads, heating, aerodynamics, and performance for high-speed aircraft. The reader will benefit from the technical and programmatic lessons learned.This volume was produced in cooperation with the National Aeronautics and Space Administration.

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

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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.

Sweeping Forward

Sweeping Forward PDF Author:
Publisher:
ISBN: 9781626830080
Category : Grumman X-29A (Jet plane)
Languages : en
Pages : 328

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Book Description
The X-29 was an unusual aircraft with a truly unique silhouette. It combined many features that challenged the technologies of its day and represented special problems for the developers and the team of testers responsible for documenting its features and design goals. This book is a look at the "big picture" of what this team accomplished in a relatively fast-paced test program involving the truly unique X-29.

Aeroacoustics of Flight Vehicles

Aeroacoustics of Flight Vehicles PDF Author: Harvey H. Hubbard
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 620

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