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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Research Memorandums
 Collection: Technical Report Archive and Image Library
The effects of fuel sloshing on the lateral stability of a free-flying airplane model

The effects of fuel sloshing on the lateral stability of a free-flying airplane model

Date: June 29, 1948
Creator: Smith, Charles C., Jr.
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
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
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
Stability and control flight tests of a 0.13-scale model of the consolidated-Vultee XFY-1 airplane in take-offs, landings, and hovering flight : TED No. NACA DE 368

Stability and control flight tests of a 0.13-scale model of the consolidated-Vultee XFY-1 airplane in take-offs, landings, and hovering flight : TED No. NACA DE 368

Date: October 1, 1952
Creator: Lovell, Powell M., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flame quenching by a variable-width rectangular-slot burner as a function of pressure for various propane-oxygen-nitrogen mixtures

Flame quenching by a variable-width rectangular-slot burner as a function of pressure for various propane-oxygen-nitrogen mixtures

Date: January 28, 1954
Creator: Berlad, Abraham L
Description: Flame quenching by a variable-width rectangular-slot burner as a function of pressure for various propane-oxygen-nitrogen mixtures was investigated. It was found that for cold gas temperatures of 27 degrees C, pressures of 0.1 ro 1.0 atmosphere, and volumetric oxygen reactions of the oxidant of 0.17, 0.21, 0.30, 0.50, and 0.70, the relation between pressure p and quenching distance d is approximately given by d (unity) p (superscript -r) with r = 1, for equivalence ratios approximately equal to one. The quenching equation of Simon and Belles was tested. For equivalence ratios less than or equal to unity, this equation may by used, together with one empirical constant, to predict the observed quenching distance within 4.2 percent. The equation in it's present form does not appear to be suitable for values of the equivalence ratio greater than unity. A quantitative theoretical investigation has also been made of the error implicit in the assumption that flame quenching by plane parallel plates of infinite extent is equivalent to that of a rectangular burner. A curve is presented which relates the magnitude of this error to the length-to-width ratio of the rectangular burner.
Contributing Partner: UNT Libraries Government Documents Department
Stability and control characteristics at low speed of a modified 1/10-scale model of the MX-1554A design

Stability and control characteristics at low speed of a modified 1/10-scale model of the MX-1554A design

Date: November 19, 1953
Creator: Lockwood, Vernard E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of two-stage-turbine efficiency characteristics in terms of work and speed requirements

Analysis of two-stage-turbine efficiency characteristics in terms of work and speed requirements

Date: August 30, 1957
Creator: Stewart, Warner L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Exploratory investigation of transpiration cooling of a 40 degree double wedge using nitrogen and helium as coolants at stagnation temperatures of 1,295 to 2,910 F

Exploratory investigation of transpiration cooling of a 40 degree double wedge using nitrogen and helium as coolants at stagnation temperatures of 1,295 to 2,910 F

Date: September 1, 1957
Creator: Rashis, Bernard
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight investigation of factors affecting the choice of minimum approach speed for carrier-type landings of a swept-wing jet fighter airplane

Flight investigation of factors affecting the choice of minimum approach speed for carrier-type landings of a swept-wing jet fighter airplane

Date: September 30, 1957
Creator: Lina, Lindsay J
Description: None
Contributing Partner: UNT Libraries Government Documents Department