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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
A summary of the drag and longitudinal trim at low lift of the North American YF-100A airplane at Mach numbers from 0.75 to 1.77 as determined by flight tests of 0.11-scale rocket models

A summary of the drag and longitudinal trim at low lift of the North American YF-100A airplane at Mach numbers from 0.75 to 1.77 as determined by flight tests of 0.11-scale rocket models

Date: January 29, 1954
Creator: Blanchard, Willard S , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Summary of the flight conditions and maneuvers in which maximum wing and tail loads were experienced on a swept-wing fighter airplane

Summary of the flight conditions and maneuvers in which maximum wing and tail loads were experienced on a swept-wing fighter airplane

Date: March 30, 1955
Creator: Sadoff, Melvin
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Summary of the lift, drag, and stability of 1/10-scale rocket-boosted models of the mc donnell xf3h-1 airplane for a mach number range of 0.6 to 1.4 as affected by the operation of extensible rocket racks

Summary of the lift, drag, and stability of 1/10-scale rocket-boosted models of the mc donnell xf3h-1 airplane for a mach number range of 0.6 to 1.4 as affected by the operation of extensible rocket racks

Date: January 1, 1954
Creator: Crabill, N. L. & Mc Fall, J. C., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Summary of the lift, drag, and stability of 1/10-scale rocket-boosted models of the McDonnell XF3H-1 airplane for a Mach number range of 0.6 to 1.4 as affected by the operation of extensible rocket racks : TED No. NACA DE 351

Summary of the lift, drag, and stability of 1/10-scale rocket-boosted models of the McDonnell XF3H-1 airplane for a Mach number range of 0.6 to 1.4 as affected by the operation of extensible rocket racks : TED No. NACA DE 351

Date: January 26, 1954
Creator: Crabill, Norman L & Mcfall, John C , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9

A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9

Date: February 27, 1957
Creator: Mitcham, Grady L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9

A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9

Date: February 27, 1957
Creator: Mitcham, G. L.
Description: Longitudinal and lateral stability and control characteristics of swept wing fighter aircraft.
Contributing Partner: UNT Libraries Government Documents Department
A summary of the low-lift drag and longitudinal trim characteristics of two versions of an interceptor-type airplane as determined from flight tests of rocket-powered models at Mach numbers between 0.75 and 1.78

A summary of the low-lift drag and longitudinal trim characteristics of two versions of an interceptor-type airplane as determined from flight tests of rocket-powered models at Mach numbers between 0.75 and 1.78

Date: November 26, 1954
Creator: Blanchard, Williard S , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Summary of the Spert-I, -II, and -III reactor facilities

Summary of the Spert-I, -II, and -III reactor facilities

Date: November 1, 1957
Creator: Montgomery, C. R.; Norberg, J. A. & Wilson, T. R.
Description: Report containing "[a] brief description and design data summary of each of the SPERT Reactor Facilities is presented. Engineering, operating, and physics data are tabulated for use as basic references" (p. 3)
Contributing Partner: UNT Libraries Government Documents Department
Summary of the theoretical lift, damping-in-roll, and center-of-pressure characteristics of various wing plan forms at supersonic speed

Summary of the theoretical lift, damping-in-roll, and center-of-pressure characteristics of various wing plan forms at supersonic speed

Date: October 1, 1949
Creator: Piland, Robert O
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Summary of Turbulence Data Obtained During United Air Lines Flight Evaluation of an Experimental C Band (5.5 cm) Airborne Weather Radar

Summary of Turbulence Data Obtained During United Air Lines Flight Evaluation of an Experimental C Band (5.5 cm) Airborne Weather Radar

Date: June 17, 1954
Creator: Coe, E. C. & Fetner, M. W.
Description: Data on atmospheric turbulence in the vicinity of thunderstorms obtained during a flight evaluation of an experimental C band (5.5 cm) airborne radar are summarized. The turbulence data were obtained with an NACA VGH recorder installed in a United Air Lines DC-3 airplane.
Contributing Partner: UNT Libraries Government Documents Department