Ask
Search
My library
ORKG

ORKG Ask

Our mission is to organize scholarly knowledge and make it accessible to humans and machines.

About

About ORKG Ask
Report issue
Statistics
Contact

Legal

Terms of use
Data protection (sheet)
Imprint
Accessibility
License

Technical

We
open source
System status
Changelog
Frontend: v1.41.0
Backend: v1.13.4

We use cookies to provide a better user experience.

Data Protection

Maximum and minimum atmospheric temperatures for aircraft design purposes

McNaughtan, I.I.
Royal Aircraft Establishment, Farnborough (UK)

Publication date

January 1958

Abstract

SIGLELD:8718.3(RAE-TN-MECH-ENG--269). / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Extracted data

Related items

World-wide extremes of humidity with temperatures between 85 degress and 120 degress F /

Cormier, René V.
Air Force Cambridge Research Laboratories (U.S.)

Design of certain Air Force systems intended for world-wide usage requires knowledge of the possible...

Procedure for scaling of experimental turbine vane airfoil temperatures from low to high gas temperatures /

Gladden, Herbert J.
Livingood, John N. B.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1971

Development of procedure for scaling of experimental turbine vane airfoil temperatures from low to h...

Further tests on the determination of the true air temperature

Wild, H
Meteorological Office, Bracknell (United Kingdom)

January 1986

Translated from German (Met. Sbor. 1887 v. 10(10))SIGLEAvailable from British Library Document Suppl...

Design temperatures for flexible airfield pavement design

Stock, A
Dundee Univ. (United Kingdom). Dept. of Civil Engineering

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:0678.231F(AD-A--214141)(microfiche) ...

Donald Bein

February 2015

Top- level military aircraft specifications typically require operational performance capability ove...

Temperatures and heat transfer on the impingement plane of a hot jet

Hampshire, R.G
Central Electricity Generating Board (CEGB), Berkeley (United Kingdom). Technology Planning and Research Div

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:3106.12862(TPRD/B--0977/R87) / BLDSC...

Developments in icing test techniques for aerospace applications in the RAE Pyestock altitude test facility

Osborn, A.
Garratt, V.
Drage, R
Defence Research Agency, Farnborough (United Kingdom). Aerospace Div

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:8670.19(RAE-TM-P--1214) / BLDSC - Br...

12.10 ESTIMATION OF U.S. DESIGN TEMPERATURES USING DAILY MAXIMUM AND MINIMUM TEMPERATURES

Kenneth E. Kunkel

March 2015

Design temperatures are commonly used for the design, sizing, distribution, installation, and market...

Optimisation of tolerances and manufacturing procedures for aircraft surface features

Sanchez, M.

January 2001

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN043133 / BLDSC - British Library D...

Airplane Design Optimization for Minimal Global Warming Impact

Proesmans, Pieter-Jan
Vos, Roelof

January 2021

This paper presents a method to assess the key performance indicators of aircraft designed for minim...

Efficient General Computational Method for Estimation of Standard Atmosphere Parameters

Daidzic, Nihad E.

March 2015

Knowledge of standard air temperature, pressure, density, speed of sound, and viscosity as a functio...

In flight heat transfer measurements on an aero-engine

Nicholas, N.
Cain, T.
Jones, T
Rolls-Royce plc (United Kingdom)

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:8019.3153(RR-PNR--92016) / BLDSC - B...

Chapter 14 Standard and Reference Atmospheres

K. S. W. Champion
A. E. Cole
A. J. Kantor

November 2014

vertical temperature profile for the portion between 32 and The World Meterological Organization (WM...

The effect of temperature on engine gas dynamics

McGinnity, F.A

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:DXN002122 / BLDSC - British Library ...

Generation of test atmospheres using an improved design of standard atmosphere system

Pengelly, M.I.
Ellwood, P.A.
Groves, J.A
Health and Safety Executive, London (United Kingdom). Research Lab. and Services Div

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:4274.8474(IR/L/SP--88/06) / BLDSC - ...

World-wide extremes of humidity with temperatures between 85 degress and 120 degress F /

Cormier, René V.
Air Force Cambridge Research Laboratories (U.S.)

Design of certain Air Force systems intended for world-wide usage requires knowledge of the possible...

Procedure for scaling of experimental turbine vane airfoil temperatures from low to high gas temperatures /

Gladden, Herbert J.
Livingood, John N. B.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1971

Development of procedure for scaling of experimental turbine vane airfoil temperatures from low to h...

Further tests on the determination of the true air temperature

Wild, H
Meteorological Office, Bracknell (United Kingdom)

January 1986

Translated from German (Met. Sbor. 1887 v. 10(10))SIGLEAvailable from British Library Document Suppl...

Design temperatures for flexible airfield pavement design

Stock, A
Dundee Univ. (United Kingdom). Dept. of Civil Engineering

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:0678.231F(AD-A--214141)(microfiche) ...

Donald Bein

February 2015

Top- level military aircraft specifications typically require operational performance capability ove...

Temperatures and heat transfer on the impingement plane of a hot jet

Hampshire, R.G
Central Electricity Generating Board (CEGB), Berkeley (United Kingdom). Technology Planning and Research Div

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:3106.12862(TPRD/B--0977/R87) / BLDSC...

Developments in icing test techniques for aerospace applications in the RAE Pyestock altitude test facility

Osborn, A.
Garratt, V.
Drage, R
Defence Research Agency, Farnborough (United Kingdom). Aerospace Div

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:8670.19(RAE-TM-P--1214) / BLDSC - Br...

12.10 ESTIMATION OF U.S. DESIGN TEMPERATURES USING DAILY MAXIMUM AND MINIMUM TEMPERATURES

Kenneth E. Kunkel

March 2015

Design temperatures are commonly used for the design, sizing, distribution, installation, and market...

Optimisation of tolerances and manufacturing procedures for aircraft surface features

Sanchez, M.

January 2001

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN043133 / BLDSC - British Library D...

Airplane Design Optimization for Minimal Global Warming Impact

Proesmans, Pieter-Jan
Vos, Roelof

January 2021

This paper presents a method to assess the key performance indicators of aircraft designed for minim...

Efficient General Computational Method for Estimation of Standard Atmosphere Parameters

Daidzic, Nihad E.

March 2015

Knowledge of standard air temperature, pressure, density, speed of sound, and viscosity as a functio...

In flight heat transfer measurements on an aero-engine

Nicholas, N.
Cain, T.
Jones, T
Rolls-Royce plc (United Kingdom)

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:8019.3153(RR-PNR--92016) / BLDSC - B...

Chapter 14 Standard and Reference Atmospheres

K. S. W. Champion
A. E. Cole
A. J. Kantor

November 2014

vertical temperature profile for the portion between 32 and The World Meterological Organization (WM...

The effect of temperature on engine gas dynamics

McGinnity, F.A

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:DXN002122 / BLDSC - British Library ...

Generation of test atmospheres using an improved design of standard atmosphere system

Pengelly, M.I.
Ellwood, P.A.
Groves, J.A
Health and Safety Executive, London (United Kingdom). Research Lab. and Services Div

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:4274.8474(IR/L/SP--88/06) / BLDSC - ...

World-wide extremes of humidity with temperatures between 85 degress and 120 degress F /

Cormier, René V.
Air Force Cambridge Research Laboratories (U.S.)

Design of certain Air Force systems intended for world-wide usage requires knowledge of the possible...

Procedure for scaling of experimental turbine vane airfoil temperatures from low to high gas temperatures /

Gladden, Herbert J.
Livingood, John N. B.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1971

Development of procedure for scaling of experimental turbine vane airfoil temperatures from low to h...

Further tests on the determination of the true air temperature

Wild, H
Meteorological Office, Bracknell (United Kingdom)

January 1986

Translated from German (Met. Sbor. 1887 v. 10(10))SIGLEAvailable from British Library Document Suppl...