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  Partner: UNT Libraries Government Documents Department
 Collection: National Advisory Committee for Aeronautics Collection
Results 13311 - 13320 of 13,806
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Wind-Tunnel Flutter Tests at Mach Numbers up to 3.0 of Boeing Wing Models for Weapons System 110A

Wind-Tunnel Flutter Tests at Mach Numbers up to 3.0 of Boeing Wing Models for Weapons System 110A

Date: September 27, 1957
Creator: Levey, G. M.; Rainey, A. G. & Tuovila, W. J.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Total-pressure-recovery Characteristics of a Model of the Mcdonnell Xf3h-1 Inlets and Forebody in a Free Jet at a Mach Number of 1.55

Total-pressure-recovery Characteristics of a Model of the Mcdonnell Xf3h-1 Inlets and Forebody in a Free Jet at a Mach Number of 1.55

Date: January 1, 1952
Creator: Carter, H. S. & Merlet, C. F.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic aerodynamic and trim characteristics of 1/15-scale models of the convair mx-1964 airplane with indented fuselage

Transonic aerodynamic and trim characteristics of 1/15-scale models of the convair mx-1964 airplane with indented fuselage

Date: January 1, 1953
Creator: Allis, A. E.; Foss, W. E., Jr. & Swihart, J. M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind tunnel investigation at high subsonic speeds of drag at 0 deg angle of attack of swept-wing fuselage models with pylon mounted and semisubmerged missiles

Wind tunnel investigation at high subsonic speeds of drag at 0 deg angle of attack of swept-wing fuselage models with pylon mounted and semisubmerged missiles

Date: October 8, 1956
Creator: King, T. J., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at low speed of the rolling stability derivatives of a 1/10-scale model of the douglas a4d-1 airplane

Wind-tunnel investigation at low speed of the rolling stability derivatives of a 1/10-scale model of the douglas a4d-1 airplane

Date: January 1, 1954
Creator: Fletcher, H. S. & Wolhart, W. D.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind Tunnel Investigation at Low Speed of the Aerodynamic Characteristics of the Army Chemical Corps Model E112 Bomblets

Wind Tunnel Investigation at Low Speed of the Aerodynamic Characteristics of the Army Chemical Corps Model E112 Bomblets

Date: November 4, 1955
Creator: Letko, W. & Williams, J. L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at high subsonic speeds of the effects on static stability characteristics of various modifications to a swept-wing fighter-type airplane model

Wind-tunnel investigation at high subsonic speeds of the effects on static stability characteristics of various modifications to a swept-wing fighter-type airplane model

Date: April 30, 1957
Creator: Goodson, K. W.
Description: Wind tunnel investigations of effect on static stability of modifications to swept wing fighter aircraft model.
Contributing Partner: UNT Libraries Government Documents Department
A Transonic Wind-Tunnel Investigation of the Performance and of the Static Stability and Control Characteristics of a 1/15-Scale Model of the Grumman F9F-9 Airplane, Ted No. NACA DE 390

A Transonic Wind-Tunnel Investigation of the Performance and of the Static Stability and Control Characteristics of a 1/15-Scale Model of the Grumman F9F-9 Airplane, Ted No. NACA DE 390

Date: October 1, 1954
Creator: Bielat, R. P.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation at low speed of the yawing stability derivatives of a 1/10-scale model of the douglas a4d-1 airplane

Wind-tunnel investigation at low speed of the yawing stability derivatives of a 1/10-scale model of the douglas a4d-1 airplane

Date: January 1, 1954
Creator: Fletcher, H. S. & Wolhart, W. D.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-Tunnel Investigation of a 0.6-Scale Model of Hughes MX-904 Tail Surface at Supersonic Speeds. Tail Attached to a Segment of the Foreshortened Body

Wind-Tunnel Investigation of a 0.6-Scale Model of Hughes MX-904 Tail Surface at Supersonic Speeds. Tail Attached to a Segment of the Foreshortened Body

Date: May 4, 1950
Creator: Conner, D. W. & Guy, L. D.
Description: None
Contributing Partner: UNT Libraries Government Documents Department