Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 332
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1064
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1064
Book Description
NASA SP.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 232
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 232
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1148
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1148
Book Description
Technical Reports Awareness Circular : TRAC.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 764
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 764
Book Description
Facilities and Techniques for Aerodynamic Testing at Transonic Speeds and High Reynolds Number
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 450
Book Description
In September 1968, the FDP of AGARD held a specialists' meeting in Paris on transonic aerodynamics, in recognition of the fact that the absence of adequate theoretical methods and wind-tunnels of high enough Reynolds number had already led to costly shortcomings in the transonic performance of certain combat and transport aircraft. Since projected aerospace systems, military, civil and space-oriented, would involve flight at Reynolds number of up to 100 million, the FDP undertook an examination of the requirements of NATO nations for wind tunnel facilities for testing large models at high Reynolds numbers.
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 450
Book Description
In September 1968, the FDP of AGARD held a specialists' meeting in Paris on transonic aerodynamics, in recognition of the fact that the absence of adequate theoretical methods and wind-tunnels of high enough Reynolds number had already led to costly shortcomings in the transonic performance of certain combat and transport aircraft. Since projected aerospace systems, military, civil and space-oriented, would involve flight at Reynolds number of up to 100 million, the FDP undertook an examination of the requirements of NATO nations for wind tunnel facilities for testing large models at high Reynolds numbers.
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 310
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 310
Book Description
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 850
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 850
Book Description
U.S. Government Research & Development Reports
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 212
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 212
Book Description
22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference: 02-2700 - 02-2926
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 694
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 694
Book Description
Government Reports Announcements
Author:
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1000
Book Description
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1000
Book Description