Atmospheric Gusts and Their Effect on Aircraft

Atmospheric Gusts and Their Effect on Aircraft

Date: August 1958
Creator: Walling, Waunnetta Keene
Description: This thesis investigates atmospheric gusts and their effect on aircraft.
Contributing Partner: UNT Libraries
A comparison of flight-measured carrier- approach speeds with values predicted by several different criteria for 41 fighter-type airplane configurations

A comparison of flight-measured carrier- approach speeds with values predicted by several different criteria for 41 fighter-type airplane configurations

Date: May 8, 1958
Creator: Drinkwater, F. J., III; Schlaff, B. A. & White, M. D.
Description: Comparison of flight measured carrier-approach speeds with values predicted by several different criteria for 41 fighter aircraft configurations.
Contributing Partner: UNT Libraries Government Documents Department
Analytical studies of the response to longitudinal control of three airplane configurations in landing approaches

Analytical studies of the response to longitudinal control of three airplane configurations in landing approaches

Date: April 9, 1953
Creator: Bihrle, W., Jr. & Stone, R. W., Jr.
Description: Analytical studies of response to longitudinal control of three aircraft configurations in carrier landing approaches.
Contributing Partner: UNT Libraries Government Documents Department
Effects of wing-fuselage flow fields on missile loads at subsonic speeds

Effects of wing-fuselage flow fields on missile loads at subsonic speeds

Date: June 27, 1955
Creator: Alford, W. J., Jr.
Description: Swept wing-fuselage flow fields on missile loads at subsonic speeds.
Contributing Partner: UNT Libraries Government Documents Department
Investigation of aerodynamic characteristics of an airplane configuration having tail surfaces outboard of the wing tips at Mach numbers of 2.30, 2.97, and 3.51

Investigation of aerodynamic characteristics of an airplane configuration having tail surfaces outboard of the wing tips at Mach numbers of 2.30, 2.97, and 3.51

Date: June 23, 1958
Creator: Church, J. D.; Hayes, W. C., Jr. & Sleeman, W. C., Jr.
Description: Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at supersonic speeds - wind tunnel stability test.
Contributing Partner: UNT Libraries Government Documents Department
Bell 47D1 Helicopter, manufactured by Bell Helicopter Inc., USA

Bell 47D1 Helicopter, manufactured by Bell Helicopter Inc., USA

Access: Use of this item is restricted to the UNT Community.
Date: 1945
Creator: Young, Arthur
Description: The 47D1 Bell helicopter hangs in the exhibition space in the Museum of Modern Art. The acrylic plastic bubble resembles an insect's head.
Contributing Partner: UNT College of Visual Arts + Design
Analysis of flight-determined and predicted effects of flexibility on the steady-state wing loads of the B-52 airplane

Analysis of flight-determined and predicted effects of flexibility on the steady-state wing loads of the B-52 airplane

Date: April 23, 1958
Creator: Kuhl, A. E.; Little, M. V. & Rogers, J. T.
Description: Flight-determined and predicted effects of flexibility on steady-state wing loads of B-52 airplane.
Contributing Partner: UNT Libraries Government Documents Department
Hydrodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight

Hydrodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight

Date: July 14, 1958
Creator: Coffee, C. W., Jr.
Description: Hydrodynamic characteristics of six-engine hull-type seaplane model designed for supersonic flight.
Contributing Partner: UNT Libraries Government Documents Department
Minimum drag of four versions of a swept-wing fighter airplane obtained from flight tests of rocket-boosted models at Mach numbers from 0.81 to 1.71

Minimum drag of four versions of a swept-wing fighter airplane obtained from flight tests of rocket-boosted models at Mach numbers from 0.81 to 1.71

Date: September 7, 1956
Creator: Hastings, E. C., Jr.
Description: Swept wing fighter aircraft drag coefficient reduction by configuration redesign.
Contributing Partner: UNT Libraries Government Documents Department
Low-speed investigation of the effect of small canard surfaces on the directional stability of a sweptback-wing fighter-airplane model

Low-speed investigation of the effect of small canard surfaces on the directional stability of a sweptback-wing fighter-airplane model

Date: August 23, 1956
Creator: Boisseau, P. C. & Paulson, J. W.
Description: Low-speed free flight tunnel testing of swept wing fighter aircraft for determining effect of small canard surfaces on directional stability.
Contributing Partner: UNT Libraries Government Documents Department
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