Author: Melvin Sadoff
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34
Book Description
NACA instrumentation has been installed in the X-4 airplanes to obtain stability and control data during the acceptance tests conducted by the Northrop Aircraft Corporation. This report presents data obtained on the stalling characteristics of the airplane in the clean and gear-down configurations. The center of gravity was located at approximately 18 percent of the mean aerodynamic chord during the tests.
Stall Characteristics Obtained from Flight 10 of Northrop X-4 No. 2 Airplane (USAF No. 46-677)
Author: Melvin Sadoff
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34
Book Description
NACA instrumentation has been installed in the X-4 airplanes to obtain stability and control data during the acceptance tests conducted by the Northrop Aircraft Corporation. This report presents data obtained on the stalling characteristics of the airplane in the clean and gear-down configurations. The center of gravity was located at approximately 18 percent of the mean aerodynamic chord during the tests.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34
Book Description
NACA instrumentation has been installed in the X-4 airplanes to obtain stability and control data during the acceptance tests conducted by the Northrop Aircraft Corporation. This report presents data obtained on the stalling characteristics of the airplane in the clean and gear-down configurations. The center of gravity was located at approximately 18 percent of the mean aerodynamic chord during the tests.
Stall Characteristics Obtained from Flight 10 of Northrop X-4 No. 2 Airplane (USAF No. 46-677)
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1338
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1338
Book Description
Research Abstracts
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 442
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 442
Book Description
Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 508
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 508
Book Description
Fifty Years of Flight Research
Author: David F. Fisher
Publisher:
ISBN:
Category : Transportation
Languages : en
Pages : 526
Book Description
A bibliography of Technical Reports from Dryden Research Center, 1946-1996. Dryden was a National Advisory Committee for Aeronautics (NACA) facility from to 1946-1958, when NACA became NASA (National Aeronautics and Space Administration). This bibliography encompasses both NACA and NASA publications. Illustrated with diagrams and photos. Black and white version.
Publisher:
ISBN:
Category : Transportation
Languages : en
Pages : 526
Book Description
A bibliography of Technical Reports from Dryden Research Center, 1946-1996. Dryden was a National Advisory Committee for Aeronautics (NACA) facility from to 1946-1958, when NACA became NASA (National Aeronautics and Space Administration). This bibliography encompasses both NACA and NASA publications. Illustrated with diagrams and photos. Black and white version.
A Selected Listing of NASA Scientific and Technical Reports for ...
Results Obtained During Flights 1 to 6 of the Northrop X-4 Airplane (A.F. No. 46-677)
Author: James T. Matthews
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 19
Book Description
The data presented include a time history of a complete pull-up, time histories of several level and accelerated flight runs, and the effect of dive-brake extension on the longitudinal and lateral trim.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 19
Book Description
The data presented include a time history of a complete pull-up, time histories of several level and accelerated flight runs, and the effect of dive-brake extension on the longitudinal and lateral trim.