Collection and analysis of wind-tunnel data on the characteristics of isolated tail surfaces with and without end plates

Collection and analysis of wind-tunnel data on the characteristics of isolated tail surfaces with and without end plates

Date: May 1, 1947
Creator: Bates, William R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Low-speed static longitudinal stability characteristics of a canard model having a 60 degrees triangular wing and horizontal tail

Low-speed static longitudinal stability characteristics of a canard model having a 60 degrees triangular wing and horizontal tail

Date: November 9, 1949
Creator: Bates, William R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Static stability of fuselages having a relatively flat cross section

Static stability of fuselages having a relatively flat cross section

Date: March 1, 1955
Creator: Bates, William R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight characteristics at low speed of a 1/12 scale model of the Consolidated Vultee 7002 airplane : (flying mock-up of XP-92)

Flight characteristics at low speed of a 1/12 scale model of the Consolidated Vultee 7002 airplane : (flying mock-up of XP-92)

Date: February 1, 1948
Creator: Tosti, Louis B
Description: Contains the results of an investigation in the Langley free-flight tunnel to determine the stability and control characteristics of a 1/12-scale dynamic free-flying model of the Consolidated Vultee 7002 airplane (a flying mock-up of the XP-92 airplane). The wing and vertical tail of this model were of triangular plan form with 60 degree sweepback of the leading edge. The results of both force and flight tests of the model are presented.
Contributing Partner: UNT Libraries Government Documents Department
Dynamic Stability and Control Characteristics of a Delta-Wing Vertically Rising Airplane Model in Take-Offs, Landings and Hovering Flight

Dynamic Stability and Control Characteristics of a Delta-Wing Vertically Rising Airplane Model in Take-Offs, Landings and Hovering Flight

Date: October 9, 1951
Creator: Lovell, Powell M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary investigation at low speed of downwash characteristics of small-scale sweptback wings

Preliminary investigation at low speed of downwash characteristics of small-scale sweptback wings

Date: July 1, 1947
Creator: Purser, Paul E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Dynamic stability and control characteristics of a vertically rising airplane model in hovering flight

Dynamic stability and control characteristics of a vertically rising airplane model in hovering flight

Date: February 1, 1951
Creator: Bates, William R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Additional Studies of the Stability and Controllability of an Unswept-Wing Vertically Rising Airplane Model in Hovering Flight Including Studies of Various Tethered Landing Techniques

Additional Studies of the Stability and Controllability of an Unswept-Wing Vertically Rising Airplane Model in Hovering Flight Including Studies of Various Tethered Landing Techniques

Date: November 6, 1951
Creator: Bates, William R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of the proximity of the ground on the stability and control characteristics of a vertically rising airplane model in the hovering condition

Effect of the proximity of the ground on the stability and control characteristics of a vertically rising airplane model in the hovering condition

Date: September 19, 1951
Creator: Smith, Charles C., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department