"Initial buckling of slightly curved panels under combined shear and compression." Source: Royal Aircraft Establishment. Report SME 3274
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 400
Type:
Archival materials
Date:
Dec 1943
Scope and Contents:
Leggett, D.M.A.; Royal Aircraft Establishment - Report SME 3274
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Bibliography of articles and papers on torsional vibration from the scientific and technical press issues by the British Air Ministry." Source: [British Air ministry]
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 401
Type:
Archival materials
Date:
Oct 1938
Scope and Contents:
Vibration - Torsional - Bibliography
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Japanese aircraft design and development ." Source: Air Technical Intelligence Group. Report 27
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 404
Type:
Archival materials
Date:
1 Nov 1945
Scope and Contents:
Airplanes - design; Airplanes - Japanese; Air Technical Intelligence Group - Report 27
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Twenty per cent of ultimate load factor required by British when determining strength of a structural component. Not always held to this." Source: Royal Aircraft Establishment
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 414
Type:
Archival materials
Date:
17 Jun 1943
Scope and Contents:
Airplanes - design and construction; [Leggett, D.M.A.];
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Shock transmission in beams." Source: Royal Aircraft Establishment. Report SME 3319
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 418
Type:
Archival materials
Date:
Apr 1945
Scope and Contents:
Robinson, A.; Beams; Royal Aircraft Establishment - Report SME 3319
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Effect of center of gravity position on aircraft behavior where turrets are rotated." Source: Aircraft and armament experimental establishment. Report Tech 50
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 419
Type:
Archival materials
Date:
21 Apr 1945
Scope and Contents:
Center of Gravity;
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Aerodynamic damping and dynamic stability. Peenemunde. translated from German." Source: Technical Data Section. Translation #399
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 421
Type:
Archival materials
Date:
7 Oct 1939
Scope and Contents:
Vibration - Damping; Airplanes - Design; Loading; Strength calculations; Royal Aircraft Establishment - Technical note SME 310
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Estimation of the structural accident rate from the distribution of loads and strength." Source: Royal Aircraft Establishment. Technical note SME 310
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 423
Type:
Archival materials
Date:
May 1945
Scope and Contents:
Cox, D.R.; Airplanes - Design; Loading; Strength calculations; Royal Aircraft Establishment - Technical note SME 310
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Relationship between required test factors and strength variation on the case of two types of failure." Source: Royal Aircraft Establishment. Technical note SME 308
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 424
Type:
Archival materials
Date:
Apr 1945
Scope and Contents:
Cox, D.R.; Structural Analysis; Royal Aircraft Establishment - Technical note SME 308
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Relationship between required test factors and strength variation." Source: Royal Aircraft Establishment. Report SME 3306
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 425
Type:
Archival materials
Date:
Feb 1945
Scope and Contents:
Starkey, R.D. & Cox, D.R.; jt auth; Structural Analysis; Royal Aircraft Establishment - Report SME 3306
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Choice of loads for ultimate repeated design and test conditions." Source: Royal Aircraft Establishment. Report SME 325
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 426
Type:
Archival materials
Date:
Jun 1945
Scope and Contents:
Montagnon, P.E.; Loads; Royal Aircraft Establishment - Report SME 325
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Simplified method of calculating dynamic loads in airplanes under given impulsive loads." Source: Royal Aircraft Establishment. Report SME 3309
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 427
Type:
Archival materials
Date:
Sep 1945
Scope and Contents:
Williams, D.; Loads; Airplanes - Design; Royal Aircraft Establishment - Report SME 3309
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Note on undercarriage loads in a banked landing." Source: Royal Aircraft Establishment. Technical Note. SME 215
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D696, Folder D52.16 / 430
Type:
Archival materials
Date:
Jan 1944
Scope and Contents:
Keogh, F.R.; Royal Aircraft Establishment. - Technical Note. SME 215
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Compression tests on dural - balsa sandwich panels." Source: Royal Aircraft Establishment. Report SME 3326
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D697, Folder D52.16 / 431
Type:
Archival materials
Date:
Jun 1945
Scope and Contents:
Chapman, R.G.; Panels - duralumin balsa; Royal Aircraft Establishment. - Report. SME 3326
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Deflection, stability & vibration of a flat rectangular panel." Source: Royal Aircraft Establishment. Report SME 3331
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D697, Folder D52.16 / 432
Type:
Archival materials
Date:
Jun 1945
Scope and Contents:
Hopkins, H.G.; Panels ; Royal Aircraft Establishment. - Report. SME 3331
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Transformation of components of stress and strain in two-dimensional elasticity." Source: Royal Aircraft Establishment. Report SME 315
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D697, Folder D52.16 / 433
Type:
Archival materials
Date:
May 1945
Scope and Contents:
Hopkins, H.G.; Elasticity; Royal Aircraft Establishment. - Report. SME 315
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"The reduction of the nose down pitching moment on underwing stores by means of a flap." Source: Royal Aircraft Establishment. Technical Note Aero 1550
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D697, Folder D52.16 / 436
Type:
Archival materials
Date:
Nov 1944
Scope and Contents:
Markowicz, M. & Walker, N.K.; jt auth; pitching moments; control; Airplanes - Hawker Typhoon; Royal Aircraft Establishment. - Technical Note Aero 1550
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
"Effect of the individual structural quantities on the flutter and aperiodic tilting of lifting surfaces with and without ailerons; without taking into account internal damping." Source: From Jahrbuch der deutschen Luftfahrtforschung, vol 1 Great Briti...
Collection Creator:
Wright-Patterson Air Force Base (Ohio) Search this
Container:
Box D697, Folder D52.16 / 441
Type:
Archival materials
Date:
1938
Scope and Contents:
Leisz, K.; Wings - vibration; Airplanes - Construction
Collection Restrictions:
No restrictions on access
Collection Rights:
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
