Pressure Measurements Obtained In Flight At Transonic Speeds For A Conically Cambered Delta Wing PDF Download

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Pressure Measurements at Transonic and Low Supersonic Speeds on a Thin Conical Cambered Low-aspect-ratio Delta Wing in Combination with Basic and Indented Bodies

Pressure Measurements at Transonic and Low Supersonic Speeds on a Thin Conical Cambered Low-aspect-ratio Delta Wing in Combination with Basic and Indented Bodies
Author: John P. Mugler
Publisher:
Total Pages: 79
Release: 1957
Genre: Aerodynamic load
ISBN:

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Pressure distributions on a thin conical cambered low-aspect-ratio delta wing have been obtained in the Langley 8-foot transonic tunnel over a Mach number range from 0.60 to 1.12 and at a Mach number of 1.43. Data were obtained for the wing in combination with a basic Sears-Haack body and a body indented symmetrically for a Mach number of 1.2. The angle-of-attack range was from -4 to 20 degrees in most instances.


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author:
Publisher:
Total Pages: 1126
Release: 1987
Genre: Aeronautics
ISBN:

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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.


NASA Technical Memorandum

NASA Technical Memorandum
Author:
Publisher:
Total Pages: 516
Release: 1976
Genre: Aeronautics
ISBN:

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NASA SP.

NASA SP.
Author:
Publisher:
Total Pages: 1426
Release: 1962
Genre: Aeronautics
ISBN:

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Total Pages: 1440
Release: 1966
Genre: Aeronautics
ISBN:

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