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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Results 15231 - 15240 of 18,906
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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
Some factors affecting the stability and performance characteristics of canard aircraft configurations

Some factors affecting the stability and performance characteristics of canard aircraft configurations

Date: June 23, 1958
Creator: Spearman, M Leroy & Driver, Cornelius
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tests of aerodynamically heated multiweb wing structures in a free jet at Mach number 2 and aluminum-alloy model of 40-inch chord with 0.125-inch-thick skin

Tests of aerodynamically heated multiweb wing structures in a free jet at Mach number 2 and aluminum-alloy model of 40-inch chord with 0.125-inch-thick skin

Date: June 23, 1958
Creator: Griffith, George E & Miltonberger, Georgene H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of a 45 deg swept wing fighter airplane model and aerodynamic loads on adjacent stores and missiles at Mach numbers of 1.57, 1.87, 2.16, and 2.53

Aerodynamic characteristics of a 45 deg swept wing fighter airplane model and aerodynamic loads on adjacent stores and missiles at Mach numbers of 1.57, 1.87, 2.16, and 2.53

Date: June 24, 1958
Creator: Oehman, W. I. & Turner, K. L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of a 45 degree swept-wing fighter-airplane model and aerodynamic loads on adjacent stores and missiles at Mach numbers of 1.57, 1.87, 2.16, and 2.53

Aerodynamic characteristics of a 45 degree swept-wing fighter-airplane model and aerodynamic loads on adjacent stores and missiles at Mach numbers of 1.57, 1.87, 2.16, and 2.53

Date: June 24, 1958
Creator: Oehman, Waldo I & Turner, Kenneth L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of several jet-spoiler controls on a 45 degree sweptback wing at Mach numbers of 1.61 and 2.01

Aerodynamic characteristics of several jet-spoiler controls on a 45 degree sweptback wing at Mach numbers of 1.61 and 2.01

Date: June 24, 1958
Creator: Lord, Douglas R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calculation of the Lateral Stability of a Directly Coupled Tandem-Towed Fighter Airplane and Correlation with Experimental Data

Calculation of the Lateral Stability of a Directly Coupled Tandem-Towed Fighter Airplane and Correlation with Experimental Data

Date: June 24, 1958
Creator: Shanks, Robert E.
Description: A theoretical method is presented for predicting the dynamic lateral stability characteristics of an airplane towed in tandem by a much larger airplane. Values of period and time to damp to one-half amplitude and rolling motions calculated by an analog computer have been correlated with results of two experimental investigations conducted in the Langley free-flight tunnel which were part of a U.S. Air Force program (Project FICON) to develop a satisfactory arrangement by which a bomber could tow a parasite fighter. In general, the theoretical results agree with the experimental results.
Contributing Partner: UNT Libraries Government Documents Department
An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers from 3.0 to 6.3

An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers from 3.0 to 6.3

Date: June 24, 1958
Creator: Gloria, H. R.
Description: Static longitudinal stability and control characteristics of wingless missile configuration at supersonic and hypersonic speeds.
Contributing Partner: UNT Libraries Government Documents Department
Some effects of mass ratio on the transonic flutter characteristics of untapered 45 degree sweptback wings of aspect ratios 2 and 3.5

Some effects of mass ratio on the transonic flutter characteristics of untapered 45 degree sweptback wings of aspect ratios 2 and 3.5

Date: June 24, 1958
Creator: Kelly, H Neale
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Exploratory Investigation of Performance of Experimental Fuelrich Hydrogen Combustion System

Exploratory Investigation of Performance of Experimental Fuelrich Hydrogen Combustion System

Date: June 25, 1958
Creator: Grobman, J. S. & Smith, A. L.
Description: Exploratory investigation of performance characteristics of fuel-rich hydrogen combustor.
Contributing Partner: UNT Libraries Government Documents Department