Access
Serial/Series Title
Language
4 Matching Results
Results open in a new window/tab.
Results:
1 - 4 of
4
Investigation at Mach Number 1.91 of Spreading Characteristics of Jet Expanding From Choked Nozzles
Report presenting an investigation at Mach number 1.91 to determine the gross spreading characteristics of jets expanding from convergent and convergent-divergent nozzles using total-temperature surveys. Results regarding the preliminary development and jet spreading characteristics of the different types of nozzles are provided.
Date:
February 11, 1952
Creator:
Rousso, Morris D. & Baughman, L. Eugene
System:
The UNT Digital Library
Longitudinal Frequency-Response Characteristics of the Douglas D-558-I Airplane as Determined From Experimental Transient-Response Histories to Mach Number of 0.90
Report presenting information regarding transient oscillations observed in response to elevator pulses of the Douglas D-558-I airplane at a range of Mach numbers and altitudes. An application of the Fourier transform was used to obtain the frequency-response characteristics. The effects of lift coefficient on the frequency response are also included.
Date:
February 11, 1952
Creator:
Angle, Ellwyn E. & Holleman, Euclid C.
System:
The UNT Digital Library
Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 2 triangular wing and an all-movable horizontal tail : lateral characteristics
Report presenting an investigation to determine the low-speed lateral characteristics of a triangular-wing airplane model. The model consisted of an aspect ratio 2 triangular wing in combination with a fuselage of fineness ratio 12.5, a thin, triangular, vertical tail with a constant-chord rudder, and a thin, unswept, all-movable horizontal tail.
Date:
February 11, 1952
Creator:
Graham, David & Koenig, David G.
System:
The UNT Digital Library
Time Histories of Maneuvers Performed With an F-86A Airplane During Squadron Operations
Report presenting some preliminary time-history results of maneuvers performed during US Air Force squadron operations with an F-86A jet-fighter airplane. The information covers a speed range from stall to 530 mph-indicated airspeed and pressure altitudes varying from sea level to approximately 25,000 feet.
Date:
February 11, 1952
Creator:
Hamer, Harold A. & Henderson, Campbell
System:
The UNT Digital Library