Skip to main content
University Libraries
Digital Collections
Home
About
Research
Services
Spaces
News
Calendar
Ask Us
Accounts
Login
Serial/Series Title
NACA Research Memorandums
34
Serial/Series Title
Sort Serial/Series Title
Sort Count
NACA Research Memorandums
34
Year
1950
34
Year
Sort Year
Sort Count
1950
34
Month
May
34
Month
Sort Month
Sort Count
May
34
Day
31st
2
29th
1
26th
3
25th
1
23rd
2
22nd
2
19th
2
18th
2
12th
1
11th
2
7 More
Day
Sort Day
Sort Count
31st
2
29th
1
26th
3
25th
1
23rd
2
22nd
2
19th
2
18th
2
12th
1
11th
2
9th
1
8th
3
5th
4
4th
2
3rd
1
2nd
3
1st
1
University Libraries
Digital Collections
Results
34 Matching Results
Your Search Terms:
Look in:
Full Text
Full Text
Metadata
Title
Subject
Creator
Names
Search
Start Over
Serial/Series Title
NACA Research Memorandums
Year
1950
Month
May
Results open in a new window/tab.
Results:
1 - 24 of 34
next
Sort by Date Created (Newest)
Best Match
Title
Creator
Date Created (Newest)
Date Created (Oldest)
Date Added (Newest)
Date Added (Oldest)
Application of blade cooling to gas turbines
Effect of Nose Shape and Wing Thickness Ratio on the Drag at Zero Lift of a Missile Having Triangular Wings and Tails
Investigation of the Spin and Recovery Characteristics of a 0.057-Scale Model of the Modified Chance Vought XF7U-1 Airplane. TED No. NACA DE 311
Fabrication and Properties of Hot-Pressed Molybdenum Disilicide
Flight Investigation of the Aileron Characteristics of the Douglas D-558-I Airplane (BuAero No. 37972) at Mach Numbers Between 0.6 and 0.89
Wing-dropping characteristics of some straight and swept wings at transonic speeds as determined with rocket-powered models
Effects of inlet icing on performance of axial-flow turbojet engine in natural icing conditions
An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degree Sweepback: A Pressure-Distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.59
Rolling Effectiveness of a Thin Tapered Wing Having Partial-Span Ailerons as Determined by Rocket-Powered Test Vehicles
Investigation of Performance of Axial-Flow Compressor of XT-46 Turbine-Propeller Engine 1 - Preliminary Investigation at 50-,70-, and 100-Percent Design Equivalent Speed
Investigation of stage performance of X24C-2 ten-stage axial-flow compressor at design speed
Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Static Lateral and Directional Stability Characteristics as Measured in Sideslips at Mach Numbers Up to 0.87
Wind-tunnel investigation at low speed to determine aerodynamic properties of a jettisonable nose section with circular cross section
Ditching Tests With a 1/16-Size Model of the Navy XP2V-1 Airplane at the Langley Tank No. 2 Monorail
Pressure Distributions on the Blade Sections of the NACA 10-(0)(066)-03 Propeller Under Operating Conditions
Flight Investigation of Longitudinal Stability and Control Characteristics and Stalling Characteristics of a C-54D Airplane
Calculated Performance of Nuclear Turbojet Powered Airplane at Flight Mach Number of 0.9
High-Subsonic Performance Characteristics and Boundary-Layer Investigations of a 12 10-Inch-Inlet-Diameter Conical Diffuser
Wind-Tunnel Investigation at Low Speed of a Wing Swept-Back 63 Degrees and Twisted and Cambered for a Uniform Load at a Lift Coefficient of 0.5
Aerodynamic characteristics of a wing with unswept quarter-chord line, aspect ratio 4, taper ratio 0.6, and NACA 65A004 airfoil section: Transonic-bump method
Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness of an elevon as a longitudinal control and the effects of camber and twist on the maximum lift-drag ratio at supersonic speeds
Characteristics of perforated diffusers at free-stream Mach number 1.90
Aerodynamic and Lateral-Control Characteristics of a 1/28-Scale Model of the Bell X-1 Airplane Wing-Fuselage Combination: Transonic-Bump Method
Aerodynamic Characteristics at a Mach Number of 1.25 of a 6-Percent-Thick Triangular Wing and 6- and 9-Percent-Thick Triangular Wings in Combination With a Fuselage: Wing Aspect Ratio 2.31, Biconvex Airfoil Sections
FIRST
PREV
1
2
NEXT
LAST
UNT Quicklinks
Search
UNT Homepage
MyUNT
Canvas
EagleConnect
UNT Directory
UNT Map
Jobs at UNT
People & Places
Information For
...
Specific Audiences
Info for
Graduate Students
Info for
Faculty/Staff
Info for
Community & Visitors
Info for
Persons with Disabilities
Locations & Hours
Willis Library
Willis Library Hours
Willis Library Location and Floor Maps
Discovery Park Library
Discovery Park Library Hours
Discovery Park Library Location and Floor Maps
Sycamore Library
Sycamore Library Hours
Sycamore Library Location and Floor Maps
Media Library
Media Library Hours
Media Library Location and Floor Maps
Spaces
Study Spaces, Classrooms, etc.
Student Room Reservations
Faculty/Staff Event Reservations
eSports Station Registration
Service Desks
Librarians and Staff
Ask Us
Departmental / Staff Directory
Subject Librarians
Employment Opportunities
Lending & Technology
Borrowing and Renewals
Catalog:
Your Account / Renew Materials
Info on Borrowing, Fines, etc.
Online Holds / Material Delivery
Technology
24 Commons, Computer Workstations
Laptop Checkout
Printing, Scanning, Photocopies
The Spark (Makerspace, Tech. Lending)
On/Off Campus Access
Help
Citations/Style Guides
Subjects
Search for a Subject or Subject Guide
Submit
Courses
Search for a Course Guide
Submit
Search, Find, Explore
Search
Full Text Online:
Summon:
Peer-Reviewed Articles, etc.
Library Catalog:
Catalog:
Basic Search
Catalog:
Advanced Search
Databases & e-Journals
Find a Database
Submit
e-Journals
Courses & Reserves
Catalog:
Course Reserves
Digital Audio Reserves
Created and/or Curated @ UNT
University Libraries Curated:
Digital Collections
UNT
Digital Library
|
TX
Portal to Texas History
|
OK
Gateway to Oklahoma History
Special Collections Finding Aids
Special Collections
Exhibits
UNT Press
Menu
CALL
The Libraries
ASK US
Account
LOGIN
University Libraries Home
Libraries:
About
Libraries:
Research
Libraries:
Services
Libraries:
Spaces
Libraries:
News
Libraries:
Calendar
facebook
twitter
instagram
github
youtube