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 Serial/Series Title: NACA Research Memorandums
 Collection: National Advisory Committee for Aeronautics Collection
Internal performance of two-dimensional wedge exhaust nozzles

Internal performance of two-dimensional wedge exhaust nozzles

Date: February 28, 1957
Creator: Beale, William T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight-determined induction-system and surge characteristics of the YF-102 airplane with a two-spool turbojet engine

Flight-determined induction-system and surge characteristics of the YF-102 airplane with a two-spool turbojet engine

Date: June 28, 1957
Creator: Saltzman, Edwin J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Hydrodynamic investigation of a model of a supersonic multijet water-based aircraft with engines exhausting from the step

Hydrodynamic investigation of a model of a supersonic multijet water-based aircraft with engines exhausting from the step

Date: August 23, 1957
Creator: Blanchard, Ulysse J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary analysis of over-all performance of an eight-stage axial -flow research compressor with two long-chord transonic inlet stages

Preliminary analysis of over-all performance of an eight-stage axial -flow research compressor with two long-chord transonic inlet stages

Date: February 10, 1958
Creator: Sievers, Gilbert K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface

Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface

Date: December 12, 1957
Creator: Johnson, Virgil E , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Component performance investigation of J71 experimental turbine VIII : effect of first-stator adjustment; internal flow conditions of J71-97 turbine with 70-percent-design stator area

Component performance investigation of J71 experimental turbine VIII : effect of first-stator adjustment; internal flow conditions of J71-97 turbine with 70-percent-design stator area

Date: September 14, 1956
Creator: Petrash, Donald A
Description: Results of a survey investigation of the J71-97 experimental three-stage turbine equipped with a first-stator area 70 percent pf design are presented and compared with the turbine with a first-stator area 97 percent of design.
Contributing Partner: UNT Libraries Government Documents Department
Experimental investigation of performance of single-stage transonic compressor with guide vanes turning counter to direction of rotor whirl

Experimental investigation of performance of single-stage transonic compressor with guide vanes turning counter to direction of rotor whirl

Date: April 22, 1957
Creator: Jahnsen, Lawrence J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Hinge-moment characteristics for a series of controls and balancing devices on a 60 degree delta wing at Mach numbers of 1.61 and 2.01

Hinge-moment characteristics for a series of controls and balancing devices on a 60 degree delta wing at Mach numbers of 1.61 and 2.01

Date: April 12, 1957
Creator: Lord, Douglas R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Longitudinal and lateral stability and control characteristics at Mach number 2.01 of a 60 degree delta-wing airplane configuration equipped with a canard control and with wing trailing-edge flap controls

Longitudinal and lateral stability and control characteristics at Mach number 2.01 of a 60 degree delta-wing airplane configuration equipped with a canard control and with wing trailing-edge flap controls

Date: March 10, 1958
Creator: Spearman, M Leroy
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Time-history data of maneuvers performed by a Republic F-84F airplane during squadron operational training

Time-history data of maneuvers performed by a Republic F-84F airplane during squadron operational training

Date: July 22, 1957
Creator: Hamer, Harold A
Description: None
Contributing Partner: UNT Libraries Government Documents Department