Supersonic Aerodynamic Characteristics of Triangular Plan-form Models at Angles of Attack to 90 Degrees PDF Download

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Supersonic Aerodynamic Characteristics of Triangular Plan-form Models at Angles of Attack to 90 Degrees

Supersonic Aerodynamic Characteristics of Triangular Plan-form Models at Angles of Attack to 90 Degrees PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

Book Description


Supersonic Aerodynamic Characteristics of Triangular Plan-form Models at Angles of Attack to 90 Degrees

Supersonic Aerodynamic Characteristics of Triangular Plan-form Models at Angles of Attack to 90 Degrees PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

Book Description


Supersonic Aerodynamic Characteristics of Some Reentry Concepts for Angles of Attack to 90 Deg

Supersonic Aerodynamic Characteristics of Some Reentry Concepts for Angles of Attack to 90 Deg PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

Book Description


Supersonic Aerodynamic Characteristics of Trianglular Plan Form Models at Angles of Attack to 90

Supersonic Aerodynamic Characteristics of Trianglular Plan Form Models at Angles of Attack to 90 PDF Author: Lyle E. Wiggins
Publisher:
ISBN:
Category :
Languages : en
Pages : 41

Book Description


Static Longitudinal Aerodynamic Characteristics at a Mach Number of 10.03 of Low-aspect-ratio Wing-body Configurations Suitable for Reentry

Static Longitudinal Aerodynamic Characteristics at a Mach Number of 10.03 of Low-aspect-ratio Wing-body Configurations Suitable for Reentry PDF Author: Lawrence Elwood Putnam
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 36

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 508

Book Description


The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms

The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms PDF Author: Max A. Heaslet
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 726

Book Description
A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1040

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.

An Analysis of the Delta-wing Hypersonic Stability and Control Behavior at Angles of Attack Between 30° and 90°

An Analysis of the Delta-wing Hypersonic Stability and Control Behavior at Angles of Attack Between 30° and 90° PDF Author: David E. Fetterman
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 72

Book Description


U.S. Government Research & Development Reports

U.S. Government Research & Development Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1014

Book Description


Government-wide Index to Federal Research & Development Reports

Government-wide Index to Federal Research & Development Reports PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1080

Book Description