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
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.
Description: Flight-determined and predicted effects of flexibility on steady-state wing loads of B-52 airplane.
Contributing Partner: UNT Libraries Government Documents Department
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
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
Use of Constant Diffuser Mach Number as a Control Parameter for Variable-geometry Inlets at Mach Numbers of 1.8 to 2.0

Use of Constant Diffuser Mach Number as a Control Parameter for Variable-geometry Inlets at Mach Numbers of 1.8 to 2.0

Date: November 4, 1957
Creator: Anderson, B. H.
Description: Control of variable-geometry inlets at constant mach numbers with blunt lip diffuser.
Contributing Partner: UNT Libraries Government Documents Department
Performance of an All-internal Conical Compression Inlet With Annular Throat Bleed at Mach Number 5.0

Performance of an All-internal Conical Compression Inlet With Annular Throat Bleed at Mach Number 5.0

Date: August 6, 1958
Creator: Obery, L. J.
Description: Internal compression inlet with throat bleed-off at hypersonic flow.
Contributing Partner: UNT Libraries Government Documents Department
Thrust and Pumping Characteristics of a Series of Ejectortype Exhaust Nozzles at Subsonic and Supersonic Flight Speeds

Thrust and Pumping Characteristics of a Series of Ejectortype Exhaust Nozzles at Subsonic and Supersonic Flight Speeds

Date: November 17, 1954
Creator: Hearth, D. P.
Description: Thrust and pumping characteristics of ejector-type exhaust nozzles at subsonic and supersonic speeds.
Contributing Partner: UNT Libraries Government Documents Department
Performance Characteristics of Several Divergent-shroud Aircraft Ejectors

Performance Characteristics of Several Divergent-shroud Aircraft Ejectors

Date: September 8, 1955
Creator: Beale, W. T.
Description: Performance characteristics of several divergent- shroud aircraft ejectors.
Contributing Partner: UNT Libraries Government Documents Department
Full-scale Evaluation of Some Flameholder Design Concepts for High-inlet-velocity Afterburners

Full-scale Evaluation of Some Flameholder Design Concepts for High-inlet-velocity Afterburners

Date: June 28, 1956
Creator: Braithwaite, W. M.
Description: Evaluation of flame holders for afterburners with high inlet velocity.
Contributing Partner: UNT Libraries Government Documents Department
In-flight Gains Realized by Modifying a Twin Side-inlet Induction System

In-flight Gains Realized by Modifying a Twin Side-inlet Induction System

Date: December 12, 1957
Creator: Saltzman, E. J.
Description: Modification of twin side-inlet induction system and in-flight gains.
Contributing Partner: UNT Libraries Government Documents Department
Force and Pressure Measurements on Several Canopy-fuselage Configurations at Mach Numbers 1.41 and 2.01

Force and Pressure Measurements on Several Canopy-fuselage Configurations at Mach Numbers 1.41 and 2.01

Date: December 15, 1955
Creator: Robins, A. W.
Description: Force and pressure measurements on several canopy- fuselage configurations at low supersonic speeds.
Contributing Partner: UNT Libraries Government Documents Department
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