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1001.
|
Dynamic stability and dispersion of a project mercury test capsule upon entering the atmosphere , with effects of roll rate centre of gravity diplacement, and threshold of a rate reaction control system [NASA TM X-350]
by Jaquet, Byron M. Material type:  Book; Format:
print
; Literary form:
not fiction
Description: 78p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1002.
|
An experimental study of the flutter of sails having a a delta planform tested from a macnh number of 0.1 to A mach number of 1.9 [NASA TM X-355]
by Hess, Robert W. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 39p.Publisher: Washington, D. C National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1003.
|
Wind tunnel investigationof the static and dynamicrotary stability derivativesofa fllat top wing body model at mach numbers of 2.5, 3.0 and 3.5 [NASA TM X-361]
by Lampkin, Bedford A | Endicott, Kenneth C. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 41p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1004.
|
The effects of wing plan from on the the static longitudinal aerodynamic characteristics of a flat-top hypersonicaircraft at mach numbers from 0.6 to 1.4 [NASA TM X-364]
by Treon, Stuart L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 31p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1005.
|
Investigation at mach numbers of 0.20 to 3.50 of blended wing combinations of sonic design with diamond, delta and arrow plan from [NASA TM X-372]
by Holdway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 77p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1006.
|
Investigation at mach numbers of 0.20 to 3.50 of blended wing body combinations of sonic design with diamond delta and arrow plan forms [NASA TM X
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 77p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: No items available
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1007.
|
Free flight measure
by Sommer, Simon C. Material type: Book Description: 41p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1008.
|
Free flight measurements of static and dynamic stability of models of the project mercury re-entry capsule at mach numbers 3 and 9.5 [NASA TM X-373]
by Sommer, Simon C | Short, Barbara J | Compton, Dale L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 41p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1009.
|
Evaluation of blended wing body combinations with curved plan forms at mach numbersn uoto 3.50 [NASA TM X-379]
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 69p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1010.
|
Experimental perfromance of area ratio 200,25 and 8 nozzles on JP-4 fuel and liquid oxygen rocket engine [NASA TM X-382]
by Lovell, Calvin Lowell | Lovell, J. Calvin, Samanich, Nick A. and Barnett, Donald O | Calvin, Lovell, J | Donald O,,Barnett. Material type: Book Description: 75p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1011.
|
Investigation at mach numbers of .60 to 3.50 of blended wing body combinationswith cambered and twisted wings with diamond, delta and arrow plan forms [NASA TM X-390]
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 76p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1012.
|
Heat transfer to blunt axially symmetric bodies [NASA TM X-391]
by Reller, John O. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 76p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1013.
|
The AMES atmosphere entry simulator and its application to the determination of ablative properties materials for ballistic missiles [NASA TM X-394]
: National Aeronautics and Space Administration
by Hamaker, Frank M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 46p.Publisher: Washingto, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1014.
|
Tables of interference factors for use in wind-tunnel and ground-effect calculations for VTOL-STOL aircraft
by Heyso, Harry H | Washington.National Aeronautics and Space Administration. Description: various pagings.Publisher: Washington National Aeronautics and Space Administration (NASA) 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1015.
|
A wind tunnel investigation at subsonic and low supersonic speeds of a re-entry vehicle with retractable wings [NASA TM X-398]
by Smith, Willard G. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 19p.Publisher: Washington, D. C. National Aeronautics and space administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1016.
|
Performance and analysis of seals for inerted lubrication systems of turbine engines [NASA TN D-4761]
by Johnson, Robert L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 21p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1017.
|
External loads and aircraft strength [NASA TT F-753]
by Gudkov, A.. I | Leshakov, P. S. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 384p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1973Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1018.
|
NASA TT [F-754]
: the measurement of radiation in space
by Gal'perin, Yu I | Washington.National Aeronautics and Space Administration | Gorn, L. S | Khazanov, B. I. Description: 326p.Publisher: Washington National Aeronautics and Space Administration (NASA) 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1019.
|
Entries from earth orbit that simulate accelaration stresses of manned planetary missions [NASA TN D-4847]
by Edwards, Frederick G. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 32p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1020.
|
Fatigue life of 120-mm bore ball bearings at 600 degree F with flurocarbon, polyphenyl ether and synthetic paraffinic base lubricants [NASA TN D-4850]
by Bamberger, Eric N. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 24p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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